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16-Civ-B1 Advanced Structural Analysis · May 2014

Question 3 of 9: Least work analysis of a propped beam

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Examination, May 2014, 98-Civ-B1 Advanced Structural Analysis — 3 hours, closed book (approved Sharp or Casio calculator permitted). Nine questions over seven pages: Questions 1 and 2 are compulsory (8 and 12 marks), then any two of Questions 3, 4, 5 (16 marks each) and any two of Questions 6, 7, 8, 9 (24 marks each). Six questions constitute a complete paper and total 100 marks. Marks are printed in the left margin. All nine questions are solved here, because the set is a study resource rather than a three-hour sitting.

Reference texts.

Throughout this paper end moments are quoted with the counter-clockwise-positive sign convention, the one that matches the standard six-degree-of-freedom stiffness element. In that convention the slope-deflection equation is

$$M_{ij}=\frac{2EI}{L}\bigl(2\theta_i+\theta_j-3\psi_{ij}\bigr)+\mathrm{FEM}_{ij}$$

the chord rotation is $\psi_{ij}=\bigl[(\mathbf{d}_j-\mathbf{d}_i)\cdot\mathbf{e}_2\bigr]/L$ with $\mathbf{e}_2$ the member axis turned $+90^\circ$, the fixed-end moment of a downward UDL is $\mathrm{FEM}_{i}=+wL^{2}/12$ and $\mathrm{FEM}_{j}=-wL^{2}/12$, and the ordinary sagging bending moment is recovered as $M_{\text{sag}}(i)=-M_{ij}$, $M_{\text{sag}}(j)=+M_{ji}$. Mixing this with the clockwise-positive convention of some textbooks is the single most common source of clean-looking but wrong answers on this paper.

Question 3: Least work analysis of a propped beam (16 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. A beam of constant $EI$, roller-supported at ① and encastré at ③, with an unloaded span ①–② and a uniformly distributed load over ②–③.

Given data
QuantitySymbolValue
Unloaded span, roller to point ③/2$a$3 m
Loaded span, point ② to the fixed end$b$6 m
Total span$L=a+b$9 m
Uniformly distributed load on $b$$w$1.8 kN/m
Flexural rigidity$EI$constant

Find. The bending moment and the shear force carried by the beam at the built-in support ③.

1.8 kN/m3 m6 m123
Question 3: propped cantilever, UDL over the outer 6 m only.

Approach. The beam has four reaction components and three equations, so it is once redundant. Take the roller reaction $R_1$ as the redundant, write $M(x)$ in terms of it, and impose the least-work condition $\partial U/\partial R_1=0$, which is exactly the statement that the roller does not deflect.

  1. Choose the redundant and write the moment field. Measuring $x$ from the roller and taking the left free body, the sagging moment is $M=R_1x$ for $0\le x\le a$ and $M=R_1x-\tfrac{w}{2}(x-a)^{2}$ for $a\le x\le L$, so $\partial M/\partial R_1=x$ everywhere.
  2. Impose least work. Because the roller is unyielding, the strain energy is stationary with respect to $R_1$:
  3. Evaluate the two integrals. The first is $\int_0^{9}x^{2}\,\mathrm{d}x=243$ and the second, substituting $u=x-3$, is $\tfrac{w}{2}\int_0^{6}u^{2}(u+3)\,\mathrm{d}u =0.9\,(324+216)=486$.
  4. Solve for the redundant. Dividing gives $R_1=486/243$, a pleasantly round result that is the tell-tale that the algebra is right.
  5. Recover the actions at the fixed end by statics. The total applied load is $wb=10.8$ kN, so vertical equilibrium gives $R_3=10.8-2.0=8.8$ kN, and the shear immediately to the left of ③ is the algebraic sum of everything to its left.
  6. Evaluate the moment at the fixed end. Substituting $x=9$ m in the second branch of $M(x)$ gives a hogging moment; the beam therefore sags over the first two-thirds of its length and hogs into the support.

The least-work condition is

$$\frac{\partial U}{\partial R_1}=\int_0^{L}\frac{M}{EI}\frac{\partial M}{\partial R_1}\,\mathrm{d}x=0\;\Longrightarrow\;R_1\int_0^{L}x^{2}\,\mathrm{d}x=\int_a^{L}\frac{w}{2}(x-a)^{2}x\,\mathrm{d}x$$

and substituting the two evaluated integrals,

$$R_1=\frac{486}{243}=\boxed{2.00\text{ kN}\ \uparrow}$$

With the redundant known the remaining actions follow from statics alone. At the built-in end,

$$M_3=R_1L-\frac{wb^{2}}{2}=2.00(9)-0.9(36)=\boxed{-14.4\text{ kN}\cdot\text{m}}$$ $$V_3=R_1-wb=2.00-10.8=\boxed{-8.8\text{ kN}}$$

The negative signs mean hogging and a downward-to-the-left shear respectively, i.e. the support hogs the beam by 14.4 kN·m and carries 8.8 kN of the 10.8 kN applied. Along the span the moment peaks at $+7.11$ kN·m at $x=4.11$ m and passes through zero at $x=6.92$ m.

Bending moment (sagging +ve)kN·m+7.11-14.4contraflexure123
Question 3: bending moment diagram, sagging positive.
ResultValue
Redundant roller reaction $R_1$2.00 kN upward
Reaction at the fixed end $R_3$8.80 kN upward
Bending moment at ③−14.4 kN·m (hogging)
Shear on the beam at ③−8.80 kN (8.80 kN magnitude)
Moment at ②+6.00 kN·m sagging
Maximum sagging moment+7.11 kN·m at $x=4.11$ m
Point of contraflexure$x=6.92$ m from the roller