Question 4 of 9: Least work — two-hinged portal frame under a uniform load
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams – May 2019,
07-Str-A4 Advanced Structural Analysis. Three hours, closed book (an approved Casio or
Sharp calculator is the only aid). Nine questions: #1 and #2 are compulsory,
then any two of #3, #4, #5 and any two of #6, #7, #8, #9 —
six questions constitute a complete paper and total 100 marks. Marks are printed in the left
margin (9, 11, 18, 18, 18, 22, 22, 22, 22). All nine questions are solved here,
because the set is a study resource rather than a three-hour sitting.
Reference texts. R. C. Hibbeler, Structural Analysis, 10th ed.
(slope-deflection, moment distribution, Castigliano and the force method);
A. Kassimali, Structural Analysis, 6th ed. (degrees of freedom, influence of support
settlement and lack of fit); J. C. McCormac, Structural Analysis: Using Classical and
Matrix Methods, 5th ed. (matrix formulation of the stiffness equations);
CSA S16:19 Design of Steel Structures and CSA A23.3:19 Design of Concrete
Structures for the Canadian design context in which these analyses are used.
Question 4: Least work — two-hinged portal frame under a uniform load (18 marks)
Given. A rectangular portal frame with joints numbered 1 (left base),
2 (top left), 3 (top right) and 4 (right base). Both bases are pinned. The beam 2–3 spans
18 m and carries a uniformly distributed load of 22 kN/m over its whole length; both columns are
6 m high. All three members have the same constant $EI$.
Given data
Symbol
Value
Meaning
$w$
22 kN/m
uniform load on the beam 2–3
$L$
18 m
beam span, centre to centre of columns
$h$
6 m
column height, pin to beam
$EI$
constant
same for all three members
Supports 1 and 4
pinned
two reaction components each
Find. The bending moment at each end of beam 2–3 and the
bending moment at its mid-span.
Question 4: two-hinged portal, 18 m span, 6 m columns, 22 kN/m on the beam.
Approach. The frame is once statically indeterminate, so choose the
horizontal thrust $H$ at the pins as the redundant, write the bending moment in every member as
a function of $H$, and impose the theorem of least work $\partial U/\partial H = 0$.
Confirm the degree of indeterminacy and pick the redundant. With
$m = 3$, $j = 4$ and $r = 4$ the frame is $3(3) + 4 - 3(4) = 1$ times statically indeterminate.
The structure and the loading are both symmetric about mid-span, so the vertical reactions
follow from symmetry at once:
$$V_1 = V_4 = \frac{wL}{2} = \frac{22 \times 18}{2} = \boxed{198\ \text{kN}}$$
and the single unknown left is the inward horizontal thrust $H$ shared by the two pins.
Write the moment in each member in terms of $H$. Measuring $y$
upwards from a pin, each column carries only the base thrust, so
$$M_{\text{col}} = H\,y, \qquad \frac{\partial M}{\partial H} = y$$
For the beam, measuring $x$ from joint 2, the free bending moment of a simply supported span is
reduced everywhere by the constant $H h$ that the thrust supplies:
$$M_{\text{beam}} = \frac{wL}{2}x - \frac{w x^{2}}{2} - H h,
\qquad \frac{\partial M}{\partial H} = -h$$
Impose least work. Because no external force does work through the
redundant, the strain energy is stationary with respect to it:
$$\frac{\partial U}{\partial H} = \frac{1}{EI}\int M\,\frac{\partial M}{\partial H}\,ds = 0$$
Splitting the integral into the two columns and the beam,
$$\frac{2}{EI}\int_{0}^{h}(H y)(y)\,dy
+ \frac{1}{EI}\int_{0}^{L}\left[\frac{wL x}{2} - \frac{w x^{2}}{2} - H h\right](-h)\,dx = 0$$
Carry out the integration. The column term gives $2Hh^{3}/3$. In the
beam term,
$$\int_{0}^{L}\left(\frac{wLx}{2} - \frac{wx^{2}}{2}\right)dx
= \frac{wL^{3}}{4} - \frac{wL^{3}}{6} = \frac{wL^{3}}{12}$$
so the condition becomes
$$\frac{2Hh^{3}}{3} - \frac{h\,wL^{3}}{12} + H h^{2}L = 0$$
Solving for the thrust and clearing the fractions,
$$\boxed{H = \frac{wL^{3}}{8h^{2} + 12hL}}$$
a result worth memorising for any symmetric two-hinged rectangular portal of uniform $EI$.
Evaluate the thrust. Substituting the given data,
$$H = \frac{22(18)^{3}}{8(6)^{2} + 12(6)(18)}
= \frac{22 \times 5832}{288 + 1296} = \frac{128\,304}{1584} = \boxed{81.0\ \text{kN}}$$
The thrust is inward at both pins, which is the expected sense: a portal loaded on its beam
tries to spread, and the supports push back.
Read the beam end moments. Each column carries a linear moment
running from zero at its pin to $H h$ at the joint, and joint equilibrium transfers that value
straight into the beam:
$$M_{2} = M_{3} = -H h = -(81.0)(6) = \boxed{486\ \text{kN}\cdot\text{m}\ \text{hogging}}$$
The equality of the two ends is a direct check on the symmetry of the solution.
Compute the mid-span moment and locate the contraflexure points.
At mid-span the free moment is $wL^{2}/8$, reduced by the same constant $Hh$:
$$M_{\text{mid}} = \frac{wL^{2}}{8} - H h = \frac{22(18)^{2}}{8} - 486
= 891 - 486 = \boxed{405\ \text{kN}\cdot\text{m}\ \text{sagging}}$$
Setting $M(x) = -486 + 198x - 11x^{2} = 0$ gives $x = 2.932$ m and $x = 15.068$ m, so the beam
hogs over roughly the outer 2.9 m at each end and sags over the middle 12.1 m.
Check the answer two ways. First, statics: the sum of the hogging
end moment and the sagging mid-span moment must return the free moment,
$486 + 405 = 891 = wL^{2}/8$, which it does exactly. Second, the limits: as $h \to 0$ the
formula gives $H \to wL^{2}/(12h) \to \infty$ (a very flat frame is nearly a two-hinged arch),
while as $h \to \infty$ it gives $H \to 0$ and the beam reverts to a simple span — both are
the physically correct trends.
Final results
Quantity
Value
Vertical reaction at each pin, $V$
198 kN
Horizontal thrust at each pin, $H$
81.0 kN (inward)
End moment $M_2 = M_3$ of beam 2–3
486 kN·m hogging
Mid-span moment of beam 2–3
405 kN·m sagging
Column moment
0 at the pin, 486 kN·m at the joint (linear)
Points of contraflexure in the beam
$x$ = 2.93 m and 15.07 m from joint 2
Statics check
$486 + 405 = 891 = wL^{2}/8$
Question 4: shear force and bending moment diagrams for beam 2–3.