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Chapter 5 · 3 hours

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Practice questions

Practice questions and answers

3 exam-style questions on this chapter, written for this site from the official syllabus. We haven’t found past IOE papers for this subject yet; if you have some, share them in the community.

  • Practice · 6 marks

Derive the expression tau = VQ/(Ib) for the shear stress at a level y1 above the neutral axis in a beam of any cross-section carrying a shear force V. State the assumptions used.

Answer

Assumptions

  1. Elastic, homogeneous material; the flexure formula holds.
  2. Shear stress is uniform across the width bb at the level considered, and acts parallel to the shear force.
  3. The beam is prismatic and the load acts through the shear centre in a plane of symmetry.

Derivation

  M          M+dM
  |<--- dx --->|        cut at y1; shaded area A* above it
  +-------------+  --- top fibre
  |    A*       |
  |-------------|  y1   width b
  |      NA     |
  +-------------+

Take a small element of length dxdx with bending moments MM and M+dMM + dM at its faces. The bending stress at a distance yy from the NA on the left face is σ=My/I\sigma = My/I. Consider the part of the element above the level y1y_1, with area A∗A^*.

Force on the left face: F1=∫A∗MyI dAF_1 = \int_{A^*}\dfrac{My}{I}\,dA. Force on the right face: F2=∫A∗(M+dM)yI dAF_2 = \int_{A^*}\dfrac{(M+dM)y}{I}\,dA.

Net unbalanced horizontal force:

F2−F1=dMI∫A∗y dA=dMI QF_2 - F_1 = \frac{dM}{I}\int_{A^*}y\,dA = \frac{dM}{I}\,Q

where Q=∫A∗y dA=A∗yˉ∗Q = \int_{A^*}y\,dA = A^*\bar y^* is the first moment of the area above the level about the NA.

This force is balanced by the horizontal shear force on the cut face of area b dxb\,dx:

τ b dx=dMIQ  ⇒  τ=QI b dMdx\tau\,b\,dx = \frac{dM}{I}Q \;\Rightarrow\; \tau = \frac{Q}{I\,b}\,\frac{dM}{dx}

Since dM/dx=VdM/dx = V:

τ=V QI b\boxed{\tau = \frac{V\,Q}{I\,b}}

By complementary shear, the same stress acts on the vertical plane. The stress is zero at the top and bottom fibres (where Q=0Q = 0) and is usually greatest at the neutral axis.

  • Practice · 8 marks

An I-section beam has flanges 150 mm wide and 20 mm thick, and a web 20 mm thick and 200 mm deep (overall depth 240 mm). At a certain section the shear force is 100 kN. Calculate the shear stress at the neutral axis, at the top of the web and in the flange just above the web junction, and sketch the distribution. What fraction of the shear force is carried by the web?

Answer

Section property

Overall depth 240240 mm. Moment of inertia about the NA (flanges plus web):

I=150×2403−130×200312=86.13×106 mm4I = \frac{150\times240^3 - 130\times200^3}{12} = 86.13\times10^6\ \text{mm}^4

(here 130 mm = (150−20)(150-20) is the total width of the two voids on either side of the web).

First moments of area

  • Flange area above the web junction (junction at 100 mm from NA): Af=150×20=3000A_f = 150\times20 = 3000 mm2^2, centroid at 110110 mm:
Qjunction=3000×110=330 000 mm3Q_{junction} = 3000\times110 = 330\,000\ \text{mm}^3
  • At the NA, add the web half-depth 100×20=2000100\times20 = 2000 mm2^2 at 5050 mm:
QNA=330 000+2000×50=430 000 mm3Q_{NA} = 330\,000 + 2000\times50 = 430\,000\ \text{mm}^3

Shear stresses τ=VQ/(Ib)\tau = VQ/(Ib)

Levelbb (mm)QQ (mm3^3)τ\tau (MPa)
Neutral axis20430 000100 000×430 00086.13×106×20=24.96\dfrac{100\,000\times430\,000}{86.13\times10^6\times20} = 24.96
Web, just below flange20330 000100 000×330 00086.13×106×20=19.16\dfrac{100\,000\times330\,000}{86.13\times10^6\times20} = 19.16
Flange, just above web150330 000100 000×330 00086.13×106×150=2.55\dfrac{100\,000\times330\,000}{86.13\times10^6\times150} = 2.55
Top of flange15000

The stress jumps from 2.55 to 19.16 MPa at the junction because the width changes from 150 to 20 mm.

 flange  |==|            0 - 2.6 MPa
         |  \
 web     |   )---> 19.2 (junction)
         |   )---> 25.0 (NA, maximum)
         |   )---> 19.2
 flange  |==|

Share of shear force

In the web the stress varies parabolically with yy (mm from the NA): τ(y)=VI b[330 000+b (1002−y2)2]\tau(y) = \dfrac{V}{I\,b}\left[330\,000 + \dfrac{b\,(100^2-y^2)}{2}\right]. Integrating τ b dy\tau\,b\,dy over the web (100 mm each side of the NA):

Vweb=∫τ b dy=92.1 kN≈92 % of VV_{web} = \int \tau\,b\,dy = 92.1\ \text{kN} \approx 92\ \%\ \text{of}\ V

Check with the simple estimate τavg=V/(web area)=100000/(20×240)=20.8\tau_{avg} = V/(\text{web area}) = 100000/(20\times240) = 20.8 MPa, close to the web values.

Answer: τNA=24.96\tau_{NA} = 24.96 MPa (maximum), τweb top=19.16\tau_{web\,top} = 19.16 MPa, τflange=2.55\tau_{flange} = 2.55 MPa; the web carries about 92 % of VV. The flanges carry the bending moment and the web carries almost all the shear.

  • Practice · 5 marks

Show that the maximum shear stress in a rectangular beam section is 1.5 times the average shear stress, and that in a solid circular section it is 4/3 times the average. Draw the shear stress distributions.

Answer

Rectangular section (b×hb\times h)

At a level yy above the NA the area above is b(h2−y)b\left(\frac{h}{2}-y\right) with centroid at 12(h2+y)\frac12\left(\frac{h}{2}+y\right):

Q=b(h2−y)⋅12(h2+y)=b2(h24−y2)Q = b\left(\frac h2 - y\right)\cdot\frac12\left(\frac h2+y\right) = \frac b2\left(\frac{h^2}{4}-y^2\right)

With I=bh3/12I = bh^3/12 and width bb:

τ=VQIb=6Vbh3(h24−y2)\tau = \frac{VQ}{Ib} = \frac{6V}{bh^3}\left(\frac{h^2}{4} - y^2\right)

This is a parabola: τ=0\tau = 0 at y=±h/2y = \pm h/2 and maximum at y=0y = 0:

τmax=6Vbh3⋅h24=3V2bh=1.5 τavg,τavg=Vbh\tau_{max} = \frac{6V}{bh^3}\cdot\frac{h^2}{4} = \frac{3V}{2bh} = 1.5\,\tau_{avg}, \qquad \tau_{avg} = \frac{V}{bh}

Solid circular section (diameter dd, radius rr)

At a level yy above the NA the chord has width b=2r2−y2b = 2\sqrt{r^2-y^2}. The first moment of the segment above yy is

Q=∫yr2r2−y12  y1 dy1=23 (r2−y2)3/2Q = \int_y^r 2\sqrt{r^2-y_1^2}\;y_1\,dy_1 = \frac23\,(r^2-y^2)^{3/2}

With I=πr4/4I = \pi r^4/4:

τ=VQIb=V⋅23(r2−y2)3/2πr44⋅2r2−y2=4V3πr4(r2−y2)\tau = \frac{VQ}{Ib} = \frac{V\cdot\frac23(r^2-y^2)^{3/2}}{\frac{\pi r^4}{4}\cdot2\sqrt{r^2-y^2}} = \frac{4V}{3\pi r^4}(r^2-y^2)

Maximum at y=0y = 0:

τmax=4V3πr2=43⋅Vπr2=43 τavg\tau_{max} = \frac{4V}{3\pi r^2} = \frac43\cdot\frac{V}{\pi r^2} = \frac43\,\tau_{avg}

Distributions

  Rectangle            Circle
  |-----|              |  ___  |
  |  \   \             | /   \ |
  |   )   ) max=1.5avg | )   ) | max=1.33avg
  |  /   /             | \___/ |
  |-----|              |       |

Both are parabolic, zero at the top and bottom edges and maximum at the neutral axis.

Written from the official syllabus. Questions and answers are written for this site; check them against your class notes.

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