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Principal MI and axes of section with semicircular cut-out

Short answer

Centroid at (44.13, 48.55) cm. Using parallel axis theorem, I_x=5.966×10^6, I_y=5.986×10^6, I_xy=-1.640×10^6 cm^4. Principal moments: I_max=7.617×10^6, I_min=4.336×10^6 cm^4. Principal axes through centroid at 45.17° (I_max) and -44.83° (I_min) from +x axis.

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.]

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.

✓ Answer checked by Claude Opus 5.5 (high effort)

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