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Chapter 2 · 7 hours

Geometrical Properties of Sections

IOE past exam questions

Past questions and answers

31 questions set from this chapter, 2 of them more than once; 1 is most repeated (set, or a close variant set, in 3 or more exams). Most repeated first.

  • Most repeated · 4 of 25 exams
  • Asked 4 times
  • 2076 Chaitra · 2 marks
  • 2074 Chaitra · 4 marks
  • 2072 Chaitra · 4 marks
  • 2066 Bhadra (old course) · 4 marks

Define principal moment of inertias and principal axes.

Answer

Principal axes

For a plane area, the principal axes are the pair of mutually perpendicular axes through a point (normally the centroid) about which the product of inertia is zero. They are the axes about which the moments of inertia take extreme (maximum and minimum) values. For a section with an axis of symmetry, the axis of symmetry and the axis perpendicular to it are principal axes.

Principal moments of inertia

The moments of inertia about the principal axes are called the principal moments of inertia: the maximum ImaxI_{max} about one principal axis and the minimum IminI_{min} about the other. For a section with IxI_x, IyI_y and IxyI_{xy} about the centroidal axes:

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2I_{max,min} = \frac{I_x + I_y}{2} \pm \sqrt{\left(\frac{I_x - I_y}{2}\right)^2 + I_{xy}^2}

The inclination of the principal axes to the x-axis is given by

tan⁡2θp=−2IxyIx−Iy\tan 2\theta_p = \frac{-2I_{xy}}{I_x - I_y}

Two directions, θp\theta_p and θp+90∘\theta_p + 90^\circ, satisfy this equation. Note that Imax+Imin=Ix+IyI_{max} + I_{min} = I_x + I_y (the polar moment of inertia is constant) and ImaxImin=IxIy−Ixy2I_{max}I_{min} = I_xI_y - I_{xy}^2.

  • Asked 2 times
  • 2075 Chaitra · 2 marks
  • 2075 Asoj · 2 marks

Define product of inertia.

Answer

The product of inertia of an area about a pair of perpendicular axes xx and yy is the sum, over the whole area, of the products of each elemental area and its two coordinates:

Ixy=∫xy dAI_{xy} = \int xy\,dA

Its unit is length4^4 (for example mm4^4). Unlike IxI_x and IyI_y, it may be positive, negative or zero: it is zero if either axis is an axis of symmetry, and it is positive when most of the area lies in the first and third quadrants. By the parallel-axis theorem Ixy=Iˉxy+AxˉyˉI_{xy} = \bar I_{xy} + A\bar x\bar y.

  • 2081 Bhadra · 12 marks

Find out the principal axis and principal moment of inertia for the given section. [Figure: plane section with a vertical left edge; the lower left part has a semicircular cut-out of radius 50 mm centred on the left edge; a circular hole of diameter 60 mm lies in the lower right-central part (60 mm marked); the top edge slopes down from a height of 100 mm above the x-axis at the y-axis to 50 mm above the x-axis at the right end; the right edge extends 50 mm above and 50 mm below the marked level; bottom dimension 150 mm + 50 mm; left side 100 mm above and 100 mm below the 50 mm mark; x-axis along the bottom and y-axis along the left edge.]

Answer

Dimensions and assumptions (read from the figure):

  • Overall outline (mm): vertices (0,−100), (150,−100), (150,−50), (200,−50), (200,50), (0,100); the top edge slopes from 100 mm to 50 mm above the x-axis.
  • Semicircular cut-out of radius 50 mm with its centre on the left edge at (0, −50), removed.
  • Circular hole of diameter 60 mm with centre (100, −25), removed.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in mm2mm^2, I in mm4mm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Outline+325003250089.10-7.0518.172×1078.172\times10^{7}9.822×1079.822\times10^{7}−9.348×105-9.348\times10^{5}
Semicircle cut-out−3927392721.22-50.002.454×1062.454\times10^{6}6.860×1056.860\times10^{5}00
Hole d = 60−28272827100.0-25.006.362×1056.362\times10^{5}6.362×1056.362\times10^{5}00

Centroid

A=∑Ai=25746 mm2Xˉ=∑AixiA=2.530×10625746=98.26 mmYˉ=∑AiyiA=3786925746=1.471 mm\begin{aligned} A &= \sum A_i = 25746\ \text{mm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{2.530\times10^{6}}{25746} = 98.26\ \text{mm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{37869}{25746} = 1.471\ \text{mm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Outline (+)8.408×1078.408\times10^{7}1.009×1081.009\times10^{8}1.601×1061.601\times10^{6}
Semicircle cut-out (−)−1.286×107-1.286\times10^{7}−2.399×107-2.399\times10^{7}−1.557×107-1.557\times10^{7}
Hole d = 60 (−)−2.617×106-2.617\times10^{6}−6.447×105-6.447\times10^{5}1.302×1051.302\times10^{5}
Total about centroid6.860×1076.860\times10^{7}7.631×1077.631\times10^{7}−1.384×107-1.384\times10^{7}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=7.246×107±1.437×107Imax=8.682×107 mm4,Imin=5.809×107 mm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 7.246\times10^{7}\pm1.437\times10^{7} \\ I_{max} &= 8.682\times10^{7}\ \text{mm}^4,\qquad I_{min} = 5.809\times10^{7}\ \text{mm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=2.768×107−7.709×106\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{2.768\times10^{7}}{-7.709\times10^{6}}, so 2θp=105.56∘2\theta_p = 105.56^\circ (and −74.44∘-74.44^\circ).

  • The axis of ImaxI_{max} makes 52.78° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -37.22° (perpendicular), both passing through the centroid (98.26, 1.471) measured from the reference origin.

Answer: Imax=8.682×107 mm4I_{max} = 8.682\times10^{7}\ \text{mm}^4, Imin=5.809×107 mm4I_{min} = 5.809\times10^{7}\ \text{mm}^4; principal axes through the centroid at 52.78° (for ImaxI_{max}) and -37.22° (for IminI_{min}) from the +x axis.

  • 2081 Baisakh · 2 marks

Differentiate between centre of gravity (CG) and centroid.

Answer

PointCentre of gravity (CG)Centroid
MeaningThe point through which the weight of the body actsThe geometric centre of an area, line or volume
Depends onMass distribution and gravityShape only
Applies to3-D bodies (solid, with weight)Plane areas, lines, volumes (geometric figures)
MaterialDepends on density of each partIndependent of material
CoincidenceCoincides with the centroid when the body is homogeneous (uniform density) and gravity is uniformSame as CG for a homogeneous body
Formulaxˉ=∑Wixi∑Wi\bar x = \dfrac{\sum W_ix_i}{\sum W_i}xˉ=∑Aixi∑Ai\bar x = \dfrac{\sum A_ix_i}{\sum A_i}
  • 2081 Baisakh · 10 marks

Determine the principle moment of inertia and orientation of principle axis for the section shown in the figure below about centroid, all dimensions are in mm. [Figure: composite section made of a vertical triangle at the top left (height 600, with a 600 horizontal dimension), a horizontal rectangular strip of length 1000 and 200 thick, and a lower right triangle with horizontal dimension 600 and height 600; overall dimensions: 600, 1000, 600 horizontal at the bottom, 200 and 600 vertical on the right.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in mm. Strip: 1000 × 200 (x 0 to 1000, y 0 to 200). Upper-left right triangle: vertices (0,200), (600,200), (0,800). Lower-right right triangle: vertices (1000,0), (400,0), (1000,−600).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in mm2mm^2, I in mm4mm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Strip 1000×200+2.000×1052.000\times10^{5}500.0100.06.667×1086.667\times10^{8}1.667×10101.667\times10^{10}00
Upper triangle+1.800×1051.800\times10^{5}200.0400.03.600×1093.600\times10^{9}3.600×1093.600\times10^{9}−1.800×109-1.800\times10^{9}
Lower triangle+1.800×1051.800\times10^{5}800.0-200.03.600×1093.600\times10^{9}3.600×1093.600\times10^{9}−1.800×109-1.800\times10^{9}

Centroid

A=∑Ai=5.600×105 mm2Xˉ=∑AixiA=2.800×1085.600×105=500.0 mmYˉ=∑AiyiA=5.600×1075.600×105=100.0 mm\begin{aligned} A &= \sum A_i = 5.600\times10^{5}\ \text{mm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{2.800\times10^{8}}{5.600\times10^{5}} = 500.0\ \text{mm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{5.600\times10^{7}}{5.600\times10^{5}} = 100.0\ \text{mm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Strip 1000×200 (+)6.667×1086.667\times10^{8}1.667×10101.667\times10^{10}00
Upper triangle (+)1.980×10101.980\times10^{10}1.980×10101.980\times10^{10}−1.800×1010-1.800\times10^{10}
Lower triangle (+)1.980×10101.980\times10^{10}1.980×10101.980\times10^{10}−1.800×1010-1.800\times10^{10}
Total about centroid4.027×10104.027\times10^{10}5.627×10105.627\times10^{10}−3.600×1010-3.600\times10^{10}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=4.827×1010±3.688×1010Imax=8.514×1010 mm4,Imin=1.139×1010 mm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 4.827\times10^{10}\pm3.688\times10^{10} \\ I_{max} &= 8.514\times10^{10}\ \text{mm}^4,\qquad I_{min} = 1.139\times10^{10}\ \text{mm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=7.200×1010−1.600×1010\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{7.200\times10^{10}}{-1.600\times10^{10}}, so 2θp=102.53∘2\theta_p = 102.53^\circ (and −77.47∘-77.47^\circ).

  • The axis of ImaxI_{max} makes 51.26° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -38.74° (perpendicular), both passing through the centroid (500.0, 100.0) measured from the reference origin.

Answer: Imax=8.514×1010 mm4I_{max} = 8.514\times10^{10}\ \text{mm}^4, Imin=1.139×1010 mm4I_{min} = 1.139\times10^{10}\ \text{mm}^4; principal axes through the centroid at 51.26° (for ImaxI_{max}) and -38.74° (for IminI_{min}) from the +x axis.

  • 2080 Bhadra · 12 marks

Find the principal moment of inertia, direction and position for the given section shown in figure. (All dimensions are in mm.) [Figure: composite section: a triangle on top-left of height 500 with 600 horizontal base marking, a rectangle of 200 depth, 600 dimension, 600 dimension, 200 vertical dimension and a quarter circle at the lower right.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in mm. Rectangle 1200 × 200 (x 0 to 1200, y 0 to 200); triangle above its left end with base 600 and height 500 (vertices (0,200), (600,200), (0,700)); quarter circle of radius 200 below the right end, centre at (1200, 0), occupying x 1000 to 1200, y −200 to 0.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in mm2mm^2, I in mm4mm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Rectangle 1200×200+2.400×1052.400\times10^{5}600.0100.08.000×1088.000\times10^{8}2.880×10102.880\times10^{10}00
Triangle+1.500×1051.500\times10^{5}200.0366.72.083×1092.083\times10^{9}3.000×1093.000\times10^{9}−1.250×109-1.250\times10^{9}
Quarter circle r = 200+31416314161115-84.888.781×1078.781\times10^{7}8.781×1078.781\times10^{7}−2.635×107-2.635\times10^{7}

Centroid

A=∑Ai=4.214×105 mm2Xˉ=∑AixiA=2.090×1084.214×105=496.0 mmYˉ=∑AiyiA=7.633×1074.214×105=181.1 mm\begin{aligned} A &= \sum A_i = 4.214\times10^{5}\ \text{mm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{2.090\times10^{8}}{4.214\times10^{5}} = 496.0\ \text{mm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{7.633\times10^{7}}{4.214\times10^{5}} = 181.1\ \text{mm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Rectangle 1200×200 (+)2.380×1092.380\times10^{9}3.139×10103.139\times10^{10}−2.025×109-2.025\times10^{9}
Triangle (+)7.247×1097.247\times10^{9}1.614×10101.614\times10^{10}−9.488×109-9.488\times10^{9}
Quarter circle r = 200 (+)2.311×1092.311\times10^{9}1.213×10101.213\times10^{10}−5.200×109-5.200\times10^{9}
Total about centroid1.194×10101.194\times10^{10}5.967×10105.967\times10^{10}−1.671×1010-1.671\times10^{10}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=3.580×1010±2.914×1010Imax=6.494×1010 mm4,Imin=6.667×109 mm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 3.580\times10^{10}\pm2.914\times10^{10} \\ I_{max} &= 6.494\times10^{10}\ \text{mm}^4,\qquad I_{min} = 6.667\times10^{9}\ \text{mm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=3.343×1010−4.773×1010\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{3.343\times10^{10}}{-4.773\times10^{10}}, so 2θp=145.00∘2\theta_p = 145.00^\circ (and −35.00∘-35.00^\circ).

  • The axis of ImaxI_{max} makes 72.50° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -17.50° (perpendicular), both passing through the centroid (496.0, 181.1) measured from the reference origin.

Answer: Imax=6.494×1010 mm4I_{max} = 6.494\times10^{10}\ \text{mm}^4, Imin=6.667×109 mm4I_{min} = 6.667\times10^{9}\ \text{mm}^4; principal axes through the centroid at 72.50° (for ImaxI_{max}) and -17.50° (for IminI_{min}) from the +x axis.

  • 2080 Baisakh · 12 marks

Determine principal moment of inertias about the centroid and also locate the principal axes for the following figure. [Figure: composite section in cm: top rectangle 5 cm wide with a sloping right side (a triangle of vertical height 15 cm to the right), a middle part 10 cm + 15 cm wide with 10 cm height, and a bottom rectangle 25 cm wide and 5 cm high; vertical dimensions 15 cm, 10 cm and 5 cm.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Bottom rectangle 25 × 5; middle rectangle 25 × 10 above it; top part is a trapezoid with a vertical left side of 15 cm, top width 5 cm and a sloping right side down to the full width of 25 cm (vertices (0,15), (25,15), (5,30), (0,30)).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Bottom 25×5+125.0125.012.502.500260.4260.46510651000
Middle 25×10+250.0250.012.5010.0020832083130211302100
Top trapezoid+225.0225.08.61120.833594359476917691−2396-2396

Centroid

A=∑Ai=600.0 cm2Xˉ=∑AixiA=6625600.0=11.04 cmYˉ=∑AiyiA=7500600.0=12.50 cm\begin{aligned} A &= \sum A_i = 600.0\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{6625}{600.0} = 11.04\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{7500}{600.0} = 12.50\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Bottom 25×5 (+)127601276067766776−1823-1823
Middle 25×10 (+)364636461355313553−911.5-911.5
Top trapezoid (+)192191921990209020−6953-6953
Total about centroid35625356252934929349−9687-9687

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=32487±10183Imax=42670 cm4,Imin=22304 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 32487\pm10183 \\ I_{max} &= 42670\ \text{cm}^4,\qquad I_{min} = 22304\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=193756276\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{19375}{6276}, so 2θp=72.05∘2\theta_p = 72.05^\circ (and −107.95∘-107.95^\circ).

  • The axis of ImaxI_{max} makes 36.03° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -53.97° (perpendicular), both passing through the centroid (11.04, 12.50) measured from the reference origin.

Answer: Imax=42670 cm4I_{max} = 42670\ \text{cm}^4, Imin=22304 cm4I_{min} = 22304\ \text{cm}^4; principal axes through the centroid at 36.03° (for ImaxI_{max}) and -53.97° (for IminI_{min}) from the +x axis.

  • 2079 Bhadra · 12 marks

Find out the principle axis and principle moment of inertia for the given section and verify using Mohr's circle. [Figure: section with a vertical left edge of height 300 mm + 200 mm + 200 mm, a triangular portion on top left, a quarter circle cut/added at the middle, and a rectangular base 200 mm + 200 mm + 200 mm wide.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in mm. Base rectangle 600 × 200; triangle above its left end (vertices (0,200), (400,200), (0,700)), so the left edge is 700 mm high; quarter circle of radius 200 added at the right of the triangle with centre (400, 200), occupying x 400 to 600, y 200 to 400.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in mm2mm^2, I in mm4mm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Base 600×200+1.200×1051.200\times10^{5}300.0100.04.000×1084.000\times10^{8}3.600×1093.600\times10^{9}00
Triangle+1.000×1051.000\times10^{5}133.3366.71.389×1091.389\times10^{9}8.889×1088.889\times10^{8}−5.556×108-5.556\times10^{8}
Quarter circle r = 200+3141631416484.9284.98.781×1078.781\times10^{7}8.781×1078.781\times10^{7}−2.635×107-2.635\times10^{7}

Centroid

A=∑Ai=2.514×105 mm2Xˉ=∑AixiA=6.457×1072.514×105=256.8 mmYˉ=∑AiyiA=5.762×1072.514×105=229.2 mm\begin{aligned} A &= \sum A_i = 2.514\times10^{5}\ \text{mm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{6.457\times10^{7}}{2.514\times10^{5}} = 256.8\ \text{mm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{5.762\times10^{7}}{2.514\times10^{5}} = 229.2\ \text{mm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Base 600×200 (+)2.402×1092.402\times10^{9}3.824×1093.824\times10^{9}−6.694×108-6.694\times10^{8}
Triangle (+)3.279×1093.279\times10^{9}2.414×1092.414\times10^{9}−2.253×109-2.253\times10^{9}
Quarter circle r = 200 (+)1.853×1081.853\times10^{8}1.722×1091.722\times10^{9}3.728×1083.728\times10^{8}
Total about centroid5.867×1095.867\times10^{9}7.959×1097.959\times10^{9}−2.550×109-2.550\times10^{9}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=6.913×109±2.756×109Imax=9.669×109 mm4,Imin=4.157×109 mm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 6.913\times10^{9}\pm2.756\times10^{9} \\ I_{max} &= 9.669\times10^{9}\ \text{mm}^4,\qquad I_{min} = 4.157\times10^{9}\ \text{mm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=5.100×109−2.092×109\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{5.100\times10^{9}}{-2.092\times10^{9}}, so 2θp=112.31∘2\theta_p = 112.31^\circ (and −67.69∘-67.69^\circ).

  • The axis of ImaxI_{max} makes 56.15° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -33.85° (perpendicular), both passing through the centroid (256.8, 229.2) measured from the reference origin.

Mohr's circle check

  • Centre C=(Ix+Iy2, 0)=(6.913×109, 0)C = \left(\dfrac{I_x+I_y}{2},\,0\right) = (6.913\times10^{9},\ 0); radius R=2.756×109R = 2.756\times10^{9}.
  • Plot X(Ix, Ixy)=(5.867×109, −2.550×109)X(I_x,\ I_{xy}) = (5.867\times10^{9},\ -2.550\times10^{9}) and Y(Iy, −Ixy)=(7.959×109, 2.550×109)Y(I_y,\ -I_{xy}) = (7.959\times10^{9},\ 2.550\times10^{9}); the line XY is a diameter.
  • The circle cuts the horizontal axis at Imax=9.669×109I_{max} = 9.669\times10^{9} and Imin=4.157×109I_{min} = 4.157\times10^{9}, equal to the values found analytically. The angle from CX to the ImaxI_{max} end of the horizontal diameter is 2θp=112.31∘2\theta_p = 112.31^\circ (turned from the x axis towards the principal axis in the same sense as the physical rotation).

Answer: Imax=9.669×109 mm4I_{max} = 9.669\times10^{9}\ \text{mm}^4, Imin=4.157×109 mm4I_{min} = 4.157\times10^{9}\ \text{mm}^4; principal axes through the centroid at 56.15° (for ImaxI_{max}) and -33.85° (for IminI_{min}) from the +x axis.

  • 2078 Bhadra · 12 marks

Calculate the principal moment of inertia about the centroid and locate the principal axes for the figure as shown below. [Figure: composite section: a quarter circle of radius 65 mm on top left, a rectangle 65 mm wide and 80 mm high below it, and a right-angled triangle of base 80 mm (to the right of the rectangle) and height 145 mm; dimensions 65 mm, 80 mm vertically and 65 mm, 80 mm horizontally.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in mm. Rectangle 65 × 80 (x 0 to 65, y 0 to 80); quarter circle of radius 65 on top with centre at (0, 80); right-angled triangle on the right of the rectangle: vertices (65,0), (145,0), (65,145) (base 80, height 145).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in mm2mm^2, I in mm4mm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Rectangle 65×80+5200520032.5040.002.773×1062.773\times10^{6}1.831×1061.831\times10^{6}00
Quarter circle r = 65+3318331827.59107.69.796×1059.796\times10^{5}9.796×1059.796\times10^{5}−2.940×105-2.940\times10^{5}
Triangle+5800580091.6748.336.775×1066.775\times10^{6}2.062×1062.062\times10^{6}−1.869×106-1.869\times10^{6}

Centroid

A=∑Ai=14318 mm2Xˉ=∑AixiA=7.922×10514318=55.33 mmYˉ=∑AiyiA=8.453×10514318=59.04 mm\begin{aligned} A &= \sum A_i = 14318\ \text{mm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{7.922\times10^{5}}{14318} = 55.33\ \text{mm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{8.453\times10^{5}}{14318} = 59.04\ \text{mm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Rectangle 65×80 (+)4.658×1064.658\times10^{6}4.541×1064.541\times10^{6}2.260×1062.260\times10^{6}
Quarter circle r = 65 (+)8.800×1068.800\times10^{6}3.533×1063.533\times10^{6}−4.763×106-4.763\times10^{6}
Triangle (+)7.439×1067.439\times10^{6}9.721×1069.721\times10^{6}−4.125×106-4.125\times10^{6}
Total about centroid2.090×1072.090\times10^{7}1.780×1071.780\times10^{7}−6.628×106-6.628\times10^{6}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=1.935×107±6.807×106Imax=2.615×107 mm4,Imin=1.254×107 mm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 1.935\times10^{7}\pm6.807\times10^{6} \\ I_{max} &= 2.615\times10^{7}\ \text{mm}^4,\qquad I_{min} = 1.254\times10^{7}\ \text{mm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=1.326×1073.103×106\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{1.326\times10^{7}}{3.103\times10^{6}}, so 2θp=76.82∘2\theta_p = 76.82^\circ (and −103.18∘-103.18^\circ).

  • The axis of ImaxI_{max} makes 38.41° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -51.59° (perpendicular), both passing through the centroid (55.33, 59.04) measured from the reference origin.

Answer: Imax=2.615×107 mm4I_{max} = 2.615\times10^{7}\ \text{mm}^4, Imin=1.254×107 mm4I_{min} = 1.254\times10^{7}\ \text{mm}^4; principal axes through the centroid at 38.41° (for ImaxI_{max}) and -51.59° (for IminI_{min}) from the +x axis.

  • 2078 Kartik · 12 marks

Determine principal moment of inertia and orientation of principal axes passing through the centroid. All dimensions are in centimeter. [Figure: composite section with horizontal dimensions 10, 20, 30, 50 and vertical dimensions 30, 60 (left side) and 50, 40, 50 (right side); a tall rectangle at top, a sloped left edge and a lower step on the right.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. The section is the polygon (0,0), (50,0), (50,50), (30,50), (30,90), (10,90), (0,30): base 50, left vertical edge 30, sloping edge of horizontal 10 and rise 60, top width 20, right side 50 + 40 with a 20 cm step.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Section+3400340023.3836.911.961×1061.961\times10^{6}5.794×1055.794\times10^{5}−1.870×105-1.870\times10^{5}

Centroid

A=∑Ai=3400 cm2Xˉ=∑AixiA=795003400=23.38 cmYˉ=∑AiyiA=1.255×1053400=36.91 cm\begin{aligned} A &= \sum A_i = 3400\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{79500}{3400} = 23.38\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{1.255\times10^{5}}{3400} = 36.91\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Section (+)1.961×1061.961\times10^{6}5.794×1055.794\times10^{5}−1.870×105-1.870\times10^{5}
Total about centroid1.961×1061.961\times10^{6}5.794×1055.794\times10^{5}−1.870×105-1.870\times10^{5}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=1.270×106±7.156×105Imax=1.986×106 cm4,Imin=5.546×105 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 1.270\times10^{6}\pm7.156\times10^{5} \\ I_{max} &= 1.986\times10^{6}\ \text{cm}^4,\qquad I_{min} = 5.546\times10^{5}\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=3.740×1051.381×106\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{3.740\times10^{5}}{1.381\times10^{6}}, so 2θp=15.15∘2\theta_p = 15.15^\circ (and −164.85∘-164.85^\circ).

  • The axis of ImaxI_{max} makes 7.57° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -82.43° (perpendicular), both passing through the centroid (23.38, 36.91) measured from the reference origin.

Answer: Imax=1.986×106 cm4I_{max} = 1.986\times10^{6}\ \text{cm}^4, Imin=5.546×105 cm4I_{min} = 5.546\times10^{5}\ \text{cm}^4; principal axes through the centroid at 7.57° (for ImaxI_{max}) and -82.43° (for IminI_{min}) from the +x axis.

  • 2076 Asoj · 2 marks

What is radius of gyration?

Answer

The radius of gyration kk of an area about an axis is the distance from that axis at which the whole area could be assumed concentrated at a point so that the moment of inertia remains the same:

I=Ak2⟹k=IAI = Ak^2 \quad\Longrightarrow\quad k = \sqrt{\frac{I}{A}}

Unit: length (mm, m). For example, kx=Ix/Ak_x = \sqrt{I_x/A} and ky=Iy/Ak_y = \sqrt{I_y/A}; for a rectangle b×db\times d, kx=d/12k_x = d/\sqrt{12} about the centroidal axis parallel to bb. It measures how far the area is spread from the axis and is used in column design through the slenderness ratio Le/kminL_e/k_{min}.

  • 2076 Asoj · 10 marks

Determine principal moment of inertia about the centroidal axis of following figure. [Figure: composite section: a quarter of a circle of radius 15 cm on top left, a rectangle below it 15 cm wide and 15 cm high, and a right-angled triangle on the right with base 30 cm and the same 15 cm height; vertical dimensions 15 cm and 15 cm, horizontal dimensions 15 cm and 30 cm.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Rectangle 15 × 15 (x 0 to 15, y 0 to 15); quarter circle of radius 15 above it with centre at (0, 15); right-angled triangle on the right: vertices (15,0), (45,0), (15,15).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Rectangle 15×15+225.0225.07.5007.500421942194219421900
Quarter circle r = 15+176.7176.76.36621.372778277827782778−833.8-833.8
Triangle+225.0225.025.005.000281228121125011250−2812-2812

Centroid

A=∑Ai=626.7 cm2Xˉ=∑AixiA=8438626.7=13.46 cmYˉ=∑AiyiA=6588626.7=10.51 cm\begin{aligned} A &= \sum A_i = 626.7\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{8438}{626.7} = 13.46\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{6588}{626.7} = 10.51\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Rectangle 15×15 (+)62606260122191221940424042
Quarter circle r = 15 (+)23596235961167911679−14446-14446
Triangle (+)964996494119841198−17121-17121
Total about centroid39506395066509665096−27526-27526

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=52301±30354Imax=82655 cm4,Imin=21947 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 52301\pm30354 \\ I_{max} &= 82655\ \text{cm}^4,\qquad I_{min} = 21947\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=55052−25590\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{55052}{-25590}, so 2θp=114.93∘2\theta_p = 114.93^\circ (and −65.07∘-65.07^\circ).

  • The axis of ImaxI_{max} makes 57.47° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -32.53° (perpendicular), both passing through the centroid (13.46, 10.51) measured from the reference origin.

Answer: Imax=82655 cm4I_{max} = 82655\ \text{cm}^4, Imin=21947 cm4I_{min} = 21947\ \text{cm}^4; principal axes through the centroid at 57.47° (for ImaxI_{max}) and -32.53° (for IminI_{min}) from the +x axis.

  • 2076 Chaitra · 10 marks

Determine principal moment of inertias and principal axes passing through the centroid for the following shaded area. [Figure: shaded plate 100 cm wide: the left edge slanted with horizontal dimension 30 cm, then 40 cm (containing a semicircular cut-out at the bottom middle), then 30 cm; vertical dimensions 25 cm and 25 cm (total 50 cm).]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Plate: vertices (0,0), (100,0), (100,50), (30,50) (left edge slanted, 30 cm horizontal, depth 50). Semicircular cut-out of diameter 40 cm (radius 20) on the bottom edge, centre (50, 0), removed.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Plate+4250425057.0623.538.762×1058.762\times10^{5}2.717×1062.717\times10^{6}2.629×1052.629\times10^{5}
Semicircle cut-out−628.3628.350.008.4881756117561628326283200

Centroid

A=∑Ai=3622 cm2Xˉ=∑AixiA=2.111×1053622=58.28 cmYˉ=∑AiyiA=946673622=26.14 cm\begin{aligned} A &= \sum A_i = 3622\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{2.111\times10^{5}}{3622} = 58.28\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{94667}{3622} = 26.14\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Plate (+)9.052×1059.052\times10^{5}2.724×1062.724\times10^{6}2.764×1052.764\times10^{5}
Semicircle cut-out (−)−2.133×105-2.133\times10^{5}−1.059×105-1.059\times10^{5}−91865-91865
Total about centroid6.919×1056.919\times10^{5}2.618×1062.618\times10^{6}1.846×1051.846\times10^{5}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=1.655×106±9.805×105Imax=2.635×106 cm4,Imin=6.743×105 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 1.655\times10^{6}\pm9.805\times10^{5} \\ I_{max} &= 2.635\times10^{6}\ \text{cm}^4,\qquad I_{min} = 6.743\times10^{5}\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=−3.692×105−1.926×106\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{-3.692\times10^{5}}{-1.926\times10^{6}}, so 2θp=−169.15∘2\theta_p = -169.15^\circ (and 10.85∘10.85^\circ).

  • The axis of ImaxI_{max} makes -84.57° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at 5.43° (perpendicular), both passing through the centroid (58.28, 26.14) measured from the reference origin.

Answer: Imax=2.635×106 cm4I_{max} = 2.635\times10^{6}\ \text{cm}^4, Imin=6.743×105 cm4I_{min} = 6.743\times10^{5}\ \text{cm}^4; principal axes through the centroid at -84.57° (for ImaxI_{max}) and 5.43° (for IminI_{min}) from the +x axis.

  • 2075 Chaitra · 10 marks

Calculate the principal moments of inertia of the section given in figure and their orientation. Assume horizontal and vertical axes to be the given x and y axes and the bottom left corner of the section to be the origin for the purpose of your calculation. [Figure: section made of a vertical left strip 12 cm high, a top flange, and a bottom flange; widths 6 cm, 8 cm and 10 cm overall; flange thicknesses 4 cm (top) and 2 cm (bottom); inner dimensions 6 cm and 8 cm.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm; origin O at the bottom-left corner. Bottom flange 6 × 2 (x 0 to 6, y 0 to 2); web 2 wide (x 4 to 6) from y = 2 to 8 (inner height 6); top flange 6 × 4 (x 4 to 10, y 8 to 12). Overall 10 wide, 12 high.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Bottom flange 6×2+12.0012.003.0001.0004.0004.00036.0036.0000
Web 2×6+12.0012.005.0005.00036.0036.004.0004.00000
Top flange 6×4+24.0024.007.00010.0032.0032.0072.0072.0000

Centroid

A=∑Ai=48.00 cm2Xˉ=∑AixiA=264.048.00=5.500 cmYˉ=∑AiyiA=312.048.00=6.500 cm\begin{aligned} A &= \sum A_i = 48.00\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{264.0}{48.00} = 5.500\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{312.0}{48.00} = 6.500\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Bottom flange 6×2 (+)367.0367.0111.0111.0165.0165.0
Web 2×6 (+)63.0063.007.0007.0009.0009.000
Top flange 6×4 (+)326.0326.0126.0126.0126.0126.0
Total about centroid756.0756.0244.0244.0300.0300.0

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=500.0±394.4Imax=894.4 cm4,Imin=105.6 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 500.0\pm394.4 \\ I_{max} &= 894.4\ \text{cm}^4,\qquad I_{min} = 105.6\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=−600.0512.0\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{-600.0}{512.0}, so 2θp=−49.52∘2\theta_p = -49.52^\circ (and 130.48∘130.48^\circ).

  • The axis of ImaxI_{max} makes -24.76° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at 65.24° (perpendicular), both passing through the centroid (5.500, 6.500) measured from the reference origin.

Values about the given origin

About the axes through the origin O: Ix=2784I_x = 2784, Iy=1696I_y = 1696, Ixy=2016 cm4I_{xy} = 2016\ \text{cm}^4 (see parts table with the parallel-axis theorem). Principal values about O: Imax=4328I_{max} = 4328, Imin=151.9I_{min} = 151.9 at -37.45° to the x axis.

Answer: Imax=894.4 cm4I_{max} = 894.4\ \text{cm}^4, Imin=105.6 cm4I_{min} = 105.6\ \text{cm}^4; principal axes through the centroid at -24.76° (for ImaxI_{max}) and 65.24° (for IminI_{min}) from the +x axis.

  • 2075 Asoj · 10 marks

Determine principal moment of inertia of the given figure below about the axes passing through the centroid. [Figure: stepped section with outer dimensions 100 cm high and 120 cm wide; top width 45 cm; 40 cm; 45 cm; 30 cm marked on the inner step (a notch with a sloping edge).]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Polygon (0,0), (120,0), (120,60), (75,60), (45,100), (0,100): height 100, base 120, top width 45, sloping edge 30 horizontal × 40 vertical, lower step 45 wide.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Section+9600960052.6642.086.678×1066.678\times10^{6}1.100×1071.100\times10^{7}−2.673×106-2.673\times10^{6}

Centroid

A=∑Ai=9600 cm2Xˉ=∑AixiA=5.055×1059600=52.66 cmYˉ=∑AiyiA=4.040×1059600=42.08 cm\begin{aligned} A &= \sum A_i = 9600\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{5.055\times10^{5}}{9600} = 52.66\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{4.040\times10^{5}}{9600} = 42.08\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Section (+)6.678×1066.678\times10^{6}1.100×1071.100\times10^{7}−2.673×106-2.673\times10^{6}
Total about centroid6.678×1066.678\times10^{6}1.100×1071.100\times10^{7}−2.673×106-2.673\times10^{6}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=8.840×106±3.438×106Imax=1.228×107 cm4,Imin=5.402×106 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 8.840\times10^{6}\pm3.438\times10^{6} \\ I_{max} &= 1.228\times10^{7}\ \text{cm}^4,\qquad I_{min} = 5.402\times10^{6}\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=5.346×106−4.324×106\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{5.346\times10^{6}}{-4.324\times10^{6}}, so 2θp=128.97∘2\theta_p = 128.97^\circ (and −51.03∘-51.03^\circ).

  • The axis of ImaxI_{max} makes 64.48° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -25.52° (perpendicular), both passing through the centroid (52.66, 42.08) measured from the reference origin.

Answer: Imax=1.228×107 cm4I_{max} = 1.228\times10^{7}\ \text{cm}^4, Imin=5.402×106 cm4I_{min} = 5.402\times10^{6}\ \text{cm}^4; principal axes through the centroid at 64.48° (for ImaxI_{max}) and -25.52° (for IminI_{min}) from the +x axis.

  • 2074 Chaitra · 10 marks

Determine the principle moment of inertia of the given figure. [Figure: section 140 cm wide at the top and 150 cm high; right edge notch dimensions 30 cm and 80 cm; bottom dimensions 20 cm and 90 cm; a sloping edge from the lower left step to the right notch.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Polygon (0,0), (110,0), (110,40), (140,120), (140,150), (0,150): bottom 110 (= 20 + 90), top width 140, total height 150, sloping edge 30 horizontal × 80 vertical.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Section+186001860062.5879.093.476×1073.476\times10^{7}2.518×1072.518\times10^{7}4.714×1064.714\times10^{6}

Centroid

A=∑Ai=18600 cm2Xˉ=∑AixiA=1.164×10618600=62.58 cmYˉ=∑AiyiA=1.471×10618600=79.09 cm\begin{aligned} A &= \sum A_i = 18600\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{1.164\times10^{6}}{18600} = 62.58\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{1.471\times10^{6}}{18600} = 79.09\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Section (+)3.476×1073.476\times10^{7}2.518×1072.518\times10^{7}4.714×1064.714\times10^{6}
Total about centroid3.476×1073.476\times10^{7}2.518×1072.518\times10^{7}4.714×1064.714\times10^{6}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=2.997×107±6.723×106Imax=3.669×107 cm4,Imin=2.325×107 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 2.997\times10^{7}\pm6.723\times10^{6} \\ I_{max} &= 3.669\times10^{7}\ \text{cm}^4,\qquad I_{min} = 2.325\times10^{7}\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=−9.428×1069.588×106\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{-9.428\times10^{6}}{9.588\times10^{6}}, so 2θp=−44.52∘2\theta_p = -44.52^\circ (and 135.48∘135.48^\circ).

  • The axis of ImaxI_{max} makes -22.26° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at 67.74° (perpendicular), both passing through the centroid (62.58, 79.09) measured from the reference origin.

Answer: Imax=3.669×107 cm4I_{max} = 3.669\times10^{7}\ \text{cm}^4, Imin=2.325×107 cm4I_{min} = 2.325\times10^{7}\ \text{cm}^4; principal axes through the centroid at -22.26° (for ImaxI_{max}) and 67.74° (for IminI_{min}) from the +x axis.

  • 2074 Asoj · 12 marks

Find the principal moments of inertia and directions of principal axes for the section as shown in figure below. [Figure: section in mm: a triangle at the top left of height 600, a horizontal rectangle of 300 thickness, a quarter circle at the lower right; dimensions 800, 800, 800.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in mm. Rectangle 800 × 300 (x 0 to 800, y 0 to 300); triangle above it with base 800 and height 600 (vertices (0,300), (800,300), (0,900)); quarter circle of radius 300 below the right end, centre (800, 0), occupying x 500 to 800, y −300 to 0.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in mm2mm^2, I in mm4mm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Rectangle 800×300+2.400×1052.400\times10^{5}400.0150.01.800×1091.800\times10^{9}1.280×10101.280\times10^{10}00
Triangle+2.400×1052.400\times10^{5}266.7500.04.800×1094.800\times10^{9}8.533×1098.533\times10^{9}−3.200×109-3.200\times10^{9}
Quarter circle r = 300+7068670686672.7-127.34.445×1084.445\times10^{8}4.445×1084.445\times10^{8}−1.334×108-1.334\times10^{8}

Centroid

A=∑Ai=5.507×105 mm2Xˉ=∑AixiA=2.075×1085.507×105=376.9 mmYˉ=∑AiyiA=1.470×1085.507×105=266.9 mm\begin{aligned} A &= \sum A_i = 5.507\times10^{5}\ \text{mm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{2.075\times10^{8}}{5.507\times10^{5}} = 376.9\ \text{mm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{1.470\times10^{8}}{5.507\times10^{5}} = 266.9\ \text{mm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Rectangle 800×300 (+)5.082×1095.082\times10^{9}1.293×10101.293\times10^{10}−6.486×108-6.486\times10^{8}
Triangle (+)1.784×10101.784\times10^{10}1.145×10101.145\times10^{10}−9.365×109-9.365\times10^{9}
Quarter circle r = 300 (+)1.143×10101.143\times10^{10}6.629×1096.629\times10^{9}−8.377×109-8.377\times10^{9}
Total about centroid3.435×10103.435\times10^{10}3.101×10103.101\times10^{10}−1.839×1010-1.839\times10^{10}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=3.268×1010±1.847×1010Imax=5.114×1010 mm4,Imin=1.421×1010 mm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 3.268\times10^{10}\pm1.847\times10^{10} \\ I_{max} &= 5.114\times10^{10}\ \text{mm}^4,\qquad I_{min} = 1.421\times10^{10}\ \text{mm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=3.678×10103.344×109\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{3.678\times10^{10}}{3.344\times10^{9}}, so 2θp=84.80∘2\theta_p = 84.80^\circ (and −95.20∘-95.20^\circ).

  • The axis of ImaxI_{max} makes 42.40° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -47.60° (perpendicular), both passing through the centroid (376.9, 266.9) measured from the reference origin.

Answer: Imax=5.114×1010 mm4I_{max} = 5.114\times10^{10}\ \text{mm}^4, Imin=1.421×1010 mm4I_{min} = 1.421\times10^{10}\ \text{mm}^4; principal axes through the centroid at 42.40° (for ImaxI_{max}) and -47.60° (for IminI_{min}) from the +x axis.

  • 2073 Shrawan · 8 marks

Obtain the principle moment of inertia and draw principle axes for the plane figure given below. [Figure: shaded plane figure 50 cm + 50 cm tall (100 cm total) with a semicircular cut-out at the bottom between horizontal dimensions 30 cm, 50 cm, 50 cm, 20 cm, 40 cm and a notch on the right side.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Plate (0,0), (100,0), (100,50), (70,50), (70,100), (0,100) (100 high, notch 30 × 50 at the top right). Semicircular cut-out of radius 20 on the bottom edge, centre (40, 0), removed.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Plate+8500850043.8245.596.918×1066.918\times10^{6}6.059×1066.059\times10^{6}−1.544×106-1.544\times10^{6}
Semicircle cut-out−628.3628.340.008.4881756117561628326283200

Centroid

A=∑Ai=7872 cm2Xˉ=∑AixiA=3.474×1057872=44.13 cmYˉ=∑AiyiA=3.822×1057872=48.55 cm\begin{aligned} A &= \sum A_i = 7872\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{3.474\times10^{5}}{7872} = 44.13\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{3.822\times10^{5}}{7872} = 48.55\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Plate (+)6.992×1066.992\times10^{6}6.060×1066.060\times10^{6}−1.536×106-1.536\times10^{6}
Semicircle cut-out (−)−1.026×106-1.026\times10^{6}−73542-73542−1.039×105-1.039\times10^{5}
Total about centroid5.966×1065.966\times10^{6}5.986×1065.986\times10^{6}−1.640×106-1.640\times10^{6}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=5.976×106±1.640×106Imax=7.617×106 cm4,Imin=4.336×106 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 5.976\times10^{6}\pm1.640\times10^{6} \\ I_{max} &= 7.617\times10^{6}\ \text{cm}^4,\qquad I_{min} = 4.336\times10^{6}\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=3.281×106−19840\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{3.281\times10^{6}}{-19840}, so 2θp=90.35∘2\theta_p = 90.35^\circ (and −89.65∘-89.65^\circ).

  • The axis of ImaxI_{max} makes 45.17° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -44.83° (perpendicular), both passing through the centroid (44.13, 48.55) measured from the reference origin.

Answer: Imax=7.617×106 cm4I_{max} = 7.617\times10^{6}\ \text{cm}^4, Imin=4.336×106 cm4I_{min} = 4.336\times10^{6}\ \text{cm}^4; principal axes through the centroid at 45.17° (for ImaxI_{max}) and -44.83° (for IminI_{min}) from the +x axis.

  • 2072 Chaitra · 12 marks

Determine principal moment of inertia and draw orientation of principal axes of the figure shown in figure below. [Figure: section with a sloping left edge: 50 cm top width, 20 cm; vertical dimensions 120 cm, 30 cm and 45 cm; bottom width 120 cm.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Polygon (0,0), (120,0), (120,45), (70,120), (20,120): bottom 120, height 120, top width 50, left sloping edge with horizontal 20, right vertical 45.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Section+113251132558.4852.091.225×1071.225\times10^{7}1.003×1071.003\times10^{7}−1.585×106-1.585\times10^{6}

Centroid

A=∑Ai=11325 cm2Xˉ=∑AixiA=6.622×10511325=58.48 cmYˉ=∑AiyiA=5.899×10511325=52.09 cm\begin{aligned} A &= \sum A_i = 11325\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{6.622\times10^{5}}{11325} = 58.48\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{5.899\times10^{5}}{11325} = 52.09\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Section (+)1.225×1071.225\times10^{7}1.003×1071.003\times10^{7}−1.585×106-1.585\times10^{6}
Total about centroid1.225×1071.225\times10^{7}1.003×1071.003\times10^{7}−1.585×106-1.585\times10^{6}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=1.114×107±1.934×106Imax=1.307×107 cm4,Imin=9.207×106 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 1.114\times10^{7}\pm1.934\times10^{6} \\ I_{max} &= 1.307\times10^{7}\ \text{cm}^4,\qquad I_{min} = 9.207\times10^{6}\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=3.170×1062.215×106\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{3.170\times10^{6}}{2.215\times10^{6}}, so 2θp=55.05∘2\theta_p = 55.05^\circ (and −124.95∘-124.95^\circ).

  • The axis of ImaxI_{max} makes 27.53° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -62.47° (perpendicular), both passing through the centroid (58.48, 52.09) measured from the reference origin.

Answer: Imax=1.307×107 cm4I_{max} = 1.307\times10^{7}\ \text{cm}^4, Imin=9.207×106 cm4I_{min} = 9.207\times10^{6}\ \text{cm}^4; principal axes through the centroid at 27.53° (for ImaxI_{max}) and -62.47° (for IminI_{min}) from the +x axis.

  • 2071 Chaitra · 12 marks

Determine the orientation of the principal axes and the moment of inertia about the centroidal axes of composite section as shown. [Figure: composite Z-type section: top width 8 cm + 12 cm + 8 cm; left part height 8 cm + 2 cm, a sloping edge, and right part 10 cm high.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Top flange 28 × 2 (x 0 to 28, y 8 to 10); left leg 8 × 8 below it (x 0 to 8, y 0 to 8); right leg 8 × 10 (x 20 to 28, y −2 to 8).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Flange 28×2+56.0056.0014.009.00018.6718.673659365900
Left leg 8×8+64.0064.004.0004.000341.3341.3341.3341.300
Right leg 8×10+80.0080.0024.003.000666.7666.7426.7426.700

Centroid

A=∑Ai=200.0 cm2Xˉ=∑AixiA=2960200.0=14.80 cmYˉ=∑AiyiA=1000200.0=5.000 cm\begin{aligned} A &= \sum A_i = 200.0\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{2960}{200.0} = 14.80\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{1000}{200.0} = 5.000\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Flange 28×2 (+)914.7914.736953695−179.2-179.2
Left leg 8×8 (+)405.3405.378067806691.2691.2
Right leg 8×10 (+)986.7986.771987198−1472-1472
Total about centroid230723071869918699−960.0-960.0

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=10503±8252Imax=18755 cm4,Imin=2251 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 10503\pm8252 \\ I_{max} &= 18755\ \text{cm}^4,\qquad I_{min} = 2251\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=1920−16392\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{1920}{-16392}, so 2θp=173.32∘2\theta_p = 173.32^\circ (and −6.68∘-6.68^\circ).

  • The axis of ImaxI_{max} makes 86.66° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -3.34° (perpendicular), both passing through the centroid (14.80, 5.000) measured from the reference origin.

Answer: Imax=18755 cm4I_{max} = 18755\ \text{cm}^4, Imin=2251 cm4I_{min} = 2251\ \text{cm}^4; principal axes through the centroid at 86.66° (for ImaxI_{max}) and -3.34° (for IminI_{min}) from the +x axis.

  • 2070 Chaitra · 12 marks

Find the principal axes and principal moments of inertia about axes through centroid of the given figure. Verify your results using Mohr's circle. [Figure: section 6 m wide (3 m + 3 m at the top), left edge vertical 6 m (2 m + 2 m + 2 m), with a sloping cut from the top-middle to the lower right; right side 2 m, 2 m, 2 m.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in m. Polygon (0,0), (6,0), (6,2), (3,6), (0,6): width 6, left side 6, top width 3, sloping edge from the top-middle to the right side at 2 m height.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in m2m^2, I in m4m^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Section+30.0030.002.6002.66782.6782.6776.2076.20−22.00-22.00

Centroid

A=∑Ai=30.00 m2Xˉ=∑AixiA=78.0030.00=2.600 mYˉ=∑AiyiA=80.0030.00=2.667 m\begin{aligned} A &= \sum A_i = 30.00\ \text{m}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{78.00}{30.00} = 2.600\ \text{m} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{80.00}{30.00} = 2.667\ \text{m} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Section (+)82.6782.6776.2076.20−22.00-22.00
Total about centroid82.6782.6776.2076.20−22.00-22.00

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=79.43±22.24Imax=101.7 m4,Imin=57.20 m4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 79.43\pm22.24 \\ I_{max} &= 101.7\ \text{m}^4,\qquad I_{min} = 57.20\ \text{m}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=44.006.467\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{44.00}{6.467}, so 2θp=81.64∘2\theta_p = 81.64^\circ (and −98.36∘-98.36^\circ).

  • The axis of ImaxI_{max} makes 40.82° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -49.18° (perpendicular), both passing through the centroid (2.600, 2.667) measured from the reference origin.

Mohr's circle check

  • Centre C=(Ix+Iy2, 0)=(79.43, 0)C = \left(\dfrac{I_x+I_y}{2},\,0\right) = (79.43,\ 0); radius R=22.24R = 22.24.
  • Plot X(Ix, Ixy)=(82.67, −22.00)X(I_x,\ I_{xy}) = (82.67,\ -22.00) and Y(Iy, −Ixy)=(76.20, 22.00)Y(I_y,\ -I_{xy}) = (76.20,\ 22.00); the line XY is a diameter.
  • The circle cuts the horizontal axis at Imax=101.7I_{max} = 101.7 and Imin=57.20I_{min} = 57.20, equal to the values found analytically. The angle from CX to the ImaxI_{max} end of the horizontal diameter is 2θp=81.64∘2\theta_p = 81.64^\circ (turned from the x axis towards the principal axis in the same sense as the physical rotation).

Answer: Imax=101.7 m4I_{max} = 101.7\ \text{m}^4, Imin=57.20 m4I_{min} = 57.20\ \text{m}^4; principal axes through the centroid at 40.82° (for ImaxI_{max}) and -49.18° (for IminI_{min}) from the +x axis.

  • 2069 Asar · 4 marks

State and prove parallel axis theorem for product of inertia.

Answer

Statement

The product of inertia of an area about any pair of perpendicular axes XX–YY is equal to the product of inertia about the parallel centroidal axes plus the product of the area and the coordinates of the centroid with respect to the XX–YY axes:

IXY=Ixy+A xˉ yˉI_{XY} = I_{xy} + A\,\bar x\,\bar y

where IxyI_{xy} is the product of inertia about the centroidal axes xx, yy (parallel to XX, YY), and (xˉ,yˉ)(\bar x, \bar y) are the coordinates of the centroid G in the XX–YY system, with signs.

Proof

Let dAdA be an element with coordinates (x,y)(x, y) with respect to the centroidal axes. Its coordinates with respect to the XX–YY axes are

X=x+xˉ,Y=y+yˉX = x + \bar x,\qquad Y = y + \bar y

Then

IXY=∫XY dA=∫(x+xˉ)(y+yˉ) dA=∫xy dA+yˉ∫x dA+xˉ∫y dA+xˉyˉ∫dA\begin{aligned} I_{XY} &= \int XY\,dA = \int (x + \bar x)(y + \bar y)\,dA\\ &= \int xy\,dA + \bar y\int x\,dA + \bar x\int y\,dA + \bar x\bar y\int dA \end{aligned}

Since xx and yy are measured from the centroid, ∫x dA=0\int x\,dA = 0 and ∫y dA=0\int y\,dA = 0. Also ∫xy dA=Ixy\int xy\,dA = I_{xy} and ∫dA=A\int dA = A. Therefore

IXY=Ixy+Axˉyˉ■I_{XY} = I_{xy} + A\bar x\bar y\qquad\blacksquare

For a composite section the same formula is applied to each part and the results are added: Ixy=∑(Iˉxy,i+Aidx,idy,i)I_{xy} = \sum (\bar I_{xy,i} + A_i d_{x,i}d_{y,i}).

  • 2069 Asar · 8 marks

Determine the principle moment of inertia about centrodial axis and locate the principle axes for the section shown in figure below. [Figure: rectangular block with horizontal dimensions 2 m, 3 m, 2 m, 3 m, 2 m (total 12 m [as marked]) and vertical dimensions 3 m (top) and 9 m, with a trapezoidal slot cut from the bottom to the top.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in m. Block 12 × 12 (x 0 to 12, y 0 to 12). Trapezoidal slot from the bottom edge: vertices (2,0), (10,0), (7,9), (5,9), removed (3 m of solid left above the slot).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in m2m^2, I in m4m^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Block 12×12+144.0144.06.0006.000172817281728172800
Trapezoid slot−45.0045.006.0003.600267.3267.3127.5127.500

Centroid

A=∑Ai=99.00 m2Xˉ=∑AixiA=594.099.00=6.000 mYˉ=∑AiyiA=702.099.00=7.091 m\begin{aligned} A &= \sum A_i = 99.00\ \text{m}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{594.0}{99.00} = 6.000\ \text{m} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{702.0}{99.00} = 7.091\ \text{m} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Block 12×12 (+)189918991728172800
Trapezoid slot (−)−815.7-815.7−127.5-127.500
Total about centroid108410841600160000

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=1342±258.4Imax=1600 m4,Imin=1084 m4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 1342\pm258.4 \\ I_{max} &= 1600\ \text{m}^4,\qquad I_{min} = 1084\ \text{m}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=0−516.8\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{0}{-516.8}, so 2θp=−180.00∘2\theta_p = -180.00^\circ (and 0.00∘0.00^\circ).

  • The axis of ImaxI_{max} makes -90.00° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at 0.00° (perpendicular), both passing through the centroid (6.000, 7.091) measured from the reference origin.

The section is symmetrical about the vertical axis x = 6 m, so Ixy=0I_{xy} = 0 and the centroidal x and y axes are themselves the principal axes.

Answer: Imax=1600 m4I_{max} = 1600\ \text{m}^4, Imin=1084 m4I_{min} = 1084\ \text{m}^4; principal axes through the centroid at -90.00° (for ImaxI_{max}) and 0.00° (for IminI_{min}) from the +x axis.

  • 2069 Chaitra · 12 marks

Determine the principal moment of inertia and orientation of principal axes for the composite section shown in figure below about its centroid. [Figure: L-shaped section: overall height 9 cm and overall width 12 cm; vertical leg 4.5 cm wide; horizontal leg 3 cm thick.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Horizontal leg 12 × 3 (x 0 to 12, y 0 to 3); vertical leg 4.5 × 6 above it (x 0 to 4.5, y 3 to 9). Overall 12 wide, 9 high.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Horizontal leg 12×3+36.0036.006.0001.50027.0027.00432.0432.000
Vertical leg 4.5×6+27.0027.002.2506.00081.0081.0045.5645.5600

Centroid

A=∑Ai=63.00 cm2Xˉ=∑AixiA=276.863.00=4.393 cmYˉ=∑AiyiA=216.063.00=3.429 cm\begin{aligned} A &= \sum A_i = 63.00\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{276.8}{63.00} = 4.393\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{216.0}{63.00} = 3.429\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Horizontal leg 12×3 (+)160.9160.9525.0525.0−111.6-111.6
Vertical leg 4.5×6 (+)259.5259.5169.5169.5−148.8-148.8
Total about centroid420.4420.4694.5694.5−260.4-260.4

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=557.5±294.2Imax=851.7 cm4,Imin=263.3 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 557.5\pm294.2 \\ I_{max} &= 851.7\ \text{cm}^4,\qquad I_{min} = 263.3\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=520.7−274.1\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{520.7}{-274.1}, so 2θp=117.76∘2\theta_p = 117.76^\circ (and −62.24∘-62.24^\circ).

  • The axis of ImaxI_{max} makes 58.88° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -31.12° (perpendicular), both passing through the centroid (4.393, 3.429) measured from the reference origin.

Answer: Imax=851.7 cm4I_{max} = 851.7\ \text{cm}^4, Imin=263.3 cm4I_{min} = 263.3\ \text{cm}^4; principal axes through the centroid at 58.88° (for ImaxI_{max}) and -31.12° (for IminI_{min}) from the +x axis.

  • 2068 Chaitra · 4 marks

Find from the first principle product of inertia for a right angled triangle with base 'b' and height 'h' along XX and YY axes. (base and height are collinear with XX and YY axes respectively).

Answer

Take a right-angled triangle with the right-angle corner at the origin, base bb along the xx-axis and height hh along the yy-axis. The hypotenuse has equation y=h(1−xb)y = h\left(1 - \dfrac{x}{b}\right).

 y
 h|\
  | \
  |  \
  |   \
  O----- b   x

Derivation from first principles

Take a vertical strip of width dxdx at distance xx, of height y1=h(1−xb)y_1 = h\left(1 - \dfrac{x}{b}\right). Its area is dA=y1 dxdA = y_1\,dx. The product of inertia of the strip about the xx and yy axes is obtained by applying the parallel-axis theorem to the strip (its own IxyI_{xy} is zero, as it is symmetrical about its centre line parallel to yy):

dIxy=(dA) x⋅y12=x y12 y1 dx=x y122 dxdI_{xy} = (dA)\,x\cdot\frac{y_1}{2} = x\,\frac{y_1}{2}\,y_1\,dx = \frac{x\,y_1^2}{2}\,dx

Hence

Ixy=∫0bx h22(1−xb)2dx=h22∫0b(x−2x2b+x3b2)dxI_{xy} = \int_0^b \frac{x\,h^2}{2}\left(1 - \frac{x}{b}\right)^2dx = \frac{h^2}{2}\int_0^b\left(x - \frac{2x^2}{b} + \frac{x^3}{b^2}\right)dx =h22[b22−2b23+b24]=h22⋅b212= \frac{h^2}{2}\left[\frac{b^2}{2} - \frac{2b^2}{3} + \frac{b^2}{4}\right] = \frac{h^2}{2}\cdot\frac{b^2}{12} Ixy=b2h224\boxed{I_{xy} = \frac{b^2h^2}{24}}

(positive, since the triangle lies in the first quadrant). About the centroidal axes, Iˉxy=b2h224−bh2⋅b3⋅h3=−b2h272\bar I_{xy} = \dfrac{b^2h^2}{24} - \dfrac{bh}{2}\cdot\dfrac{b}{3}\cdot\dfrac{h}{3} = -\dfrac{b^2h^2}{72}.

  • 2068 Chaitra · 8 marks

Calculate principal moment of inertia and the orientation of the principle axes for the shaded area shown in figure below. [Figure: trapezoid with vertical left side 15 cm, bottom width 10 cm + 12 cm; the top edge is 10 cm wide and the right edge slopes down to the bottom right corner.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Trapezoid (0,0), (22,0), (10,15), (0,15): vertical left side 15, bottom 10 + 12 = 22, top 10.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Trapezoid+240.0240.08.3756.5624289428965266526−1716-1716

Centroid

A=∑Ai=240.0 cm2Xˉ=∑AixiA=2010240.0=8.375 cmYˉ=∑AiyiA=1575240.0=6.562 cm\begin{aligned} A &= \sum A_i = 240.0\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{2010}{240.0} = 8.375\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{1575}{240.0} = 6.562\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Trapezoid (+)4289428965266526−1716-1716
Total about centroid4289428965266526−1716-1716

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=5408±2048Imax=7456 cm4,Imin=3360 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 5408\pm2048 \\ I_{max} &= 7456\ \text{cm}^4,\qquad I_{min} = 3360\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=3431−2237\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{3431}{-2237}, so 2θp=123.10∘2\theta_p = 123.10^\circ (and −56.90∘-56.90^\circ).

  • The axis of ImaxI_{max} makes 61.55° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -28.45° (perpendicular), both passing through the centroid (8.375, 6.562) measured from the reference origin.

Answer: Imax=7456 cm4I_{max} = 7456\ \text{cm}^4, Imin=3360 cm4I_{min} = 3360\ \text{cm}^4; principal axes through the centroid at 61.55° (for ImaxI_{max}) and -28.45° (for IminI_{min}) from the +x axis.

  • 2068 Baisakh (old course) · 12 marks

Calculate the principal moment of inertia about centroid and locate the principle axes for the figure as shown below. [Figure: section in cm: top flange 20 cm wide and 4 cm thick; web 4 cm thick and 16 cm high; bottom flange 15 cm + 15 cm wide (30 cm) and 8 cm thick; a semicircular hole of radius 4 cm at the bottom centre.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm; x measured from the vertical axis of symmetry. Bottom flange 30 × 8, web 4 × 16, top flange 20 × 4, with a semicircular hole of radius 4 on the bottom edge at the centre (diameter on the bottom face, bulging upward).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Bottom flange 30×8+240.0240.004.00012801280180001800000
Web 4×16+64.0064.00016.001365136585.3385.3300
Top flange 20×4+80.0080.00026.00106.7106.72667266700
Semicircular hole r = 4−25.1325.1301.69828.1028.10100.5100.500

Centroid

A=∑Ai=358.9 cm2Xˉ=∑AixiA=0358.9=0 cmYˉ=∑AiyiA=4021358.9=11.21 cm\begin{aligned} A &= \sum A_i = 358.9\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{0}{358.9} = 0\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{4021}{358.9} = 11.21\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Bottom flange 30×8 (+)1374113741180001800000
Web 4×16 (+)2836283685.3385.3300
Top flange 20×4 (+)17617176172667266700
Semicircular hole r = 4 (−)−2300-2300−100.5-100.500
Total about centroid3189431894206512065100

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=26273±5621Imax=31894 cm4,Imin=20651 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 26273\pm5621 \\ I_{max} &= 31894\ \text{cm}^4,\qquad I_{min} = 20651\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=011242\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{0}{11242}, so 2θp=−0.00∘2\theta_p = -0.00^\circ (and −180.00∘-180.00^\circ).

  • The axis of ImaxI_{max} makes 0.00° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at 90.00° (perpendicular), both passing through the centroid (0, 11.21) measured from the reference origin.

The section is symmetrical about the vertical axis, so Ixy=0I_{xy} = 0 and the centroidal horizontal and vertical axes are the principal axes.

Answer: Imax=31894 cm4I_{max} = 31894\ \text{cm}^4, Imin=20651 cm4I_{min} = 20651\ \text{cm}^4; principal axes through the centroid at 0.00° (for ImaxI_{max}) and 90.00° (for IminI_{min}) from the +x axis.

  • 2067 Asar (old course) · 12 marks

Calculate the principal MoI and their orientation for the following section about X-Y axes. [Figure: L-shaped section in mm with origin O at the bottom left corner; horizontal leg 60 mm long and 10 mm thick; vertical leg 12 mm wide.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in mm; origin O at the bottom-left corner. Horizontal leg 60 × 10 (x 0 to 60, y 0 to 10); vertical leg 12 × 50 above it (x 0 to 12, y 10 to 60). Both legs are 60 mm long overall.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in mm2mm^2, I in mm4mm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Horizontal leg 60×10+600.0600.030.005.000500050001.800×1051.800\times10^{5}00
Vertical leg 12×50+600.0600.06.00035.001.250×1051.250\times10^{5}7200720000

Centroid

A=∑Ai=1200 mm2Xˉ=∑AixiA=216001200=18.00 mmYˉ=∑AiyiA=240001200=20.00 mm\begin{aligned} A &= \sum A_i = 1200\ \text{mm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{21600}{1200} = 18.00\ \text{mm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{24000}{1200} = 20.00\ \text{mm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Horizontal leg 60×10 (+)1.400×1051.400\times10^{5}2.664×1052.664\times10^{5}−1.080×105-1.080\times10^{5}
Vertical leg 12×50 (+)2.600×1052.600\times10^{5}9360093600−1.080×105-1.080\times10^{5}
Total about centroid4.000×1054.000\times10^{5}3.600×1053.600\times10^{5}−2.160×105-2.160\times10^{5}

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=3.800×105±2.169×105Imax=5.969×105 mm4,Imin=1.631×105 mm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 3.800\times10^{5}\pm2.169\times10^{5} \\ I_{max} &= 5.969\times10^{5}\ \text{mm}^4,\qquad I_{min} = 1.631\times10^{5}\ \text{mm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=4.320×10540000\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{4.320\times10^{5}}{40000}, so 2θp=84.71∘2\theta_p = 84.71^\circ (and −95.29∘-95.29^\circ).

  • The axis of ImaxI_{max} makes 42.35° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -47.65° (perpendicular), both passing through the centroid (18.00, 20.00) measured from the reference origin.

Values about the given origin

About the axes through the origin O: Ix=8.800×105I_x = 8.800\times10^{5}, Iy=7.488×105I_y = 7.488\times10^{5}, Ixy=2.160×105 mm4I_{xy} = 2.160\times10^{5}\ \text{mm}^4 (see parts table with the parallel-axis theorem). Principal values about O: Imax=1.040×106I_{max} = 1.040\times10^{6}, Imin=5.887×105I_{min} = 5.887\times10^{5} at -36.55° to the x axis.

Answer: Imax=5.969×105 mm4I_{max} = 5.969\times10^{5}\ \text{mm}^4, Imin=1.631×105 mm4I_{min} = 1.631\times10^{5}\ \text{mm}^4; principal axes through the centroid at 42.35° (for ImaxI_{max}) and -47.65° (for IminI_{min}) from the +x axis.

  • 2066 Bhadra (old course) · 12 marks

Determine the orientation of principal axes and the principal moment of inertia about centroidal axes of the composite section shown in figure. [Figure: composite section in cm: left triangle of height 6 cm + 2 cm with base 6 cm; central rectangle 12 cm long; right triangle with horizontal extent 6 cm and vertical extent 7 cm.]

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Left triangle: vertices (0,0), (6,0), (6,8) (base 6, height 6 + 2). Central rectangle 12 × 6 (x 6 to 18, y 0 to 6). Right triangle: vertices (18,0), (24,0), (18,7) (horizontal 6, vertical 7).

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Left triangle+24.0024.004.0002.66785.3385.3348.0048.0032.0032.00
Rectangle 12×6+72.0072.0012.003.000216.0216.0864.0864.000
Right triangle+21.0021.0020.002.33357.1757.1742.0042.00−24.50-24.50

Centroid

A=∑Ai=117.0 cm2Xˉ=∑AixiA=1380117.0=11.79 cmYˉ=∑AiyiA=329.0117.0=2.812 cm\begin{aligned} A &= \sum A_i = 117.0\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{1380}{117.0} = 11.79\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{329.0}{117.0} = 2.812\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Left triangle (+)85.8485.841506150659.1859.18
Rectangle 12×6 (+)218.5218.5867.0867.02.7772.777
Right triangle (+)61.9861.9814561456−107.0-107.0
Total about centroid366.4366.438293829−45.01-45.01

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=2098±1732Imax=3830 cm4,Imin=365.8 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 2098\pm1732 \\ I_{max} &= 3830\ \text{cm}^4,\qquad I_{min} = 365.8\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=90.03−3463\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{90.03}{-3463}, so 2θp=178.51∘2\theta_p = 178.51^\circ (and −1.49∘-1.49^\circ).

  • The axis of ImaxI_{max} makes 89.26° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -0.74° (perpendicular), both passing through the centroid (11.79, 2.812) measured from the reference origin.

Answer: Imax=3830 cm4I_{max} = 3830\ \text{cm}^4, Imin=365.8 cm4I_{min} = 365.8\ \text{cm}^4; principal axes through the centroid at 89.26° (for ImaxI_{max}) and -0.74° (for IminI_{min}) from the +x axis.

  • 2066 Jestha (old course) · 8 marks

Calculate principal moment of inertia about the X-Y axes and locate the principal axes of the right angled triangle section with 15cm x 15cm sides. [Figure: right-angled triangle with the right angle at the origin, legs of 15 cm along the X and Y axes.]

Answer

Right angle at the origin O, legs of 15 cm along the X and Y axes (so b=h=15b = h = 15 cm). The principal axes are required for the X–Y axes at O.

 Y
15|\
  | \
  |  \
  O---- 15  X

Moments and product of inertia about X–Y

Ix=bh312=15×15312=4218.750 cm4Iy=hb312=4218.750 cm4Ixy=b2h224=152×15224=2109.375 cm4\begin{aligned} I_x &= \frac{bh^3}{12} = \frac{15\times15^3}{12} = 4218.750\ \text{cm}^4\\ I_y &= \frac{hb^3}{12} = 4218.750\ \text{cm}^4\\ I_{xy} &= \frac{b^2h^2}{24} = \frac{15^2\times15^2}{24} = 2109.375\ \text{cm}^4 \end{aligned}

Principal moments of inertia

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=4218.750±0+2109.3752Imax=6328.125 cm4,Imin=2109.375 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} = 4218.750\pm\sqrt{0 + 2109.375^2}\\ I_{max} &= 6328.125\ \text{cm}^4,\qquad I_{min} = 2109.375\ \text{cm}^4 \end{aligned}

Principal axes

tan⁡2θp=−2IxyIx−Iy=−2(2109.375)0=−∞  ⇒  2θp=−90∘ or 90∘\tan2\theta_p = \frac{-2I_{xy}}{I_x-I_y} = \frac{-2(2109.375)}{0} = -\infty\;\Rightarrow\;2\theta_p = -90^\circ\ \text{or}\ 90^\circ

so θp=45∘\theta_p = 45^\circ and 135∘135^\circ. Checking with I(θ)=Ix+Iy2+Ix−Iy2cos⁡2θ−Ixysin⁡2θI(\theta) = \frac{I_x+I_y}{2} + \frac{I_x-I_y}{2}\cos2\theta - I_{xy}\sin2\theta: at θ=135∘\theta = 135^\circ it is I=4218.750−2109.375sin⁡270∘=6328.125I = 4218.750 - 2109.375\sin270^\circ = 6328.125 (maximum), and at θ=45∘\theta = 45^\circ it is 2109.3752109.375 (minimum).

Answer: Imax=6328.12 cm4I_{max} = 6328.12\ \text{cm}^4 about the axis through O at 135∘135^\circ to X (parallel to the hypotenuse), and Imin=2109.38 cm4I_{min} = 2109.38\ \text{cm}^4 about the axis through O at 45∘45^\circ to X (the line from O to the mid-point of the hypotenuse).

  • 2066 Chaitra (old course) · 16 marks

Calculate principal moment of inertia and locate the principal axes through the centroid of the area of the L section shown in figure. Total depth of the web is 20cm. Total breadth of the flange is 15cm and thickness of the web and flange is 5cm.

Answer

Dimensions and assumptions (read from the figure):

  • Dimensions in cm. Flange 15 × 5 (x 0 to 15, y 0 to 5); web 5 × 15 above it (x 0 to 5, y 5 to 20). Total depth 20, breadth 15, thickness 5.

Properties of the parts (x, y measured from the reference origin; IGI_G about the part's own centroid; area in cm2cm^2, I in cm4cm^4)

PartSignAxˉ\bar xyˉ\bar yIx,GI_{x,G}Iy,GI_{y,G}Ixy,GI_{xy,G}
Flange 15×5+75.0075.007.5002.500156.2156.21406140600
Web 5×15+75.0075.002.50012.5014061406156.2156.200

Centroid

A=∑Ai=150.0 cm2Xˉ=∑AixiA=750.0150.0=5.000 cmYˉ=∑AiyiA=1125150.0=7.500 cm\begin{aligned} A &= \sum A_i = 150.0\ \text{cm}^2 \\ \bar X &= \frac{\sum A_i x_i}{A} = \frac{750.0}{150.0} = 5.000\ \text{cm} \\ \bar Y &= \frac{\sum A_i y_i}{A} = \frac{1125}{150.0} = 7.500\ \text{cm} \end{aligned}

Moments and product of inertia about the centroidal axes

With dx=xi−Xˉd_x = x_i-\bar X, dy=yi−Yˉd_y = y_i-\bar Y and the parallel-axis theorems Ix=Ix,G+Ady2I_x = I_{x,G}+Ad_y^2, Iy=Iy,G+Adx2I_y = I_{y,G}+Ad_x^2, Ixy=Ixy,G+AdxdyI_{xy} = I_{xy,G}+Ad_xd_y:

PartIx,G+Ady2I_{x,G}+A d_y^2Iy,G+Adx2I_{y,G}+A d_x^2Ixy,G+AdxdyI_{xy,G}+A d_x d_y
Flange 15×5 (+)2031203118751875−937.5-937.5
Web 5×15 (+)32813281625.0625.0−937.5-937.5
Total about centroid5312531225002500−1875-1875

Principal moments of inertia and principal axes

Imax,min=Ix+Iy2±(Ix−Iy2)2+Ixy2=3906±2344Imax=6250 cm4,Imin=1562 cm4\begin{aligned} I_{max,min} &= \frac{I_x+I_y}{2}\pm\sqrt{\left(\frac{I_x-I_y}{2}\right)^2+I_{xy}^2} \\ &= 3906\pm2344 \\ I_{max} &= 6250\ \text{cm}^4,\qquad I_{min} = 1562\ \text{cm}^4 \end{aligned}

Orientation: tan⁡2θp=−2IxyIx−Iy=37502812\tan 2\theta_p = \dfrac{-2I_{xy}}{I_x-I_y} = \dfrac{3750}{2812}, so 2θp=53.13∘2\theta_p = 53.13^\circ (and −126.87∘-126.87^\circ).

  • The axis of ImaxI_{max} makes 26.57° with the +x axis (anticlockwise positive); the axis of IminI_{min} is at -63.43° (perpendicular), both passing through the centroid (5.000, 7.500) measured from the reference origin.

Answer: Imax=6250 cm4I_{max} = 6250\ \text{cm}^4, Imin=1562 cm4I_{min} = 1562\ \text{cm}^4; principal axes through the centroid at 26.57° (for ImaxI_{max}) and -63.43° (for IminI_{min}) from the +x axis.

Questions from Old Question Collection (CE 502) (IOE BCE Strength of Materials exam papers, 2066 to 2081 (25 papers)). Answers are written for this site; check them against your class notes.

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