Question 8 of 8: Reactions and internal-force diagrams for a determinate portal frame with an internal hinge
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2013
— 07-Str-A1 Elementary Structural Analysis. Three hours, CLOSED BOOK, an
approved Sharp or Casio calculator permitted. Six questions constitute a complete paper:
candidates answer ALL of Questions 1 to 5 and ONE of Questions 6, 7 or 8. Marks are shown in
the left margin (6 + 18 + 18 + 18 + 20 + 20 = 100). All eight questions are solved below,
because the three alternatives test different topics and the whole set is useful for
study.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 2 (determinacy and
stability), Ch. 3 to 5 (trusses, internal loadings, frames), Ch. 6 (influence lines),
Ch. 8 to 9 (deflections and virtual work), Ch. 11 to 12 (slope-deflection and moment
distribution).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3 (equilibrium and
determinacy), Ch. 4 (plane trusses), Ch. 5 (beams and frames), Ch. 7 (deflections by virtual
work), Ch. 8 (influence lines), Ch. 16 to 17 (slope-deflection and moment distribution).
K. Leet, C.-M. Uang and A. Gilbert, Fundamentals of Structural Analysis, 5th ed.
— a parallel treatment of the same syllabus.
C. H. Norris, J. B. Wilbur and S. Utku, Elementary Structural Analysis, 4th ed.
— the classical text after which this exam code is named.
Canadian design context: CSA S16 Design of Steel Structures, CSA A23.3
Design of Concrete Structures and the National Building Code of Canada.
This is an analysis paper, so no code clause is needed to answer it, but every result below is
expressed in the SI units those documents use.
Sign conventions used throughout. For beams and for each individual frame
member, shear is positive when the resultant of the forces to the left of (or below) a section
acts upward, and bending moment is positive when it sags the member, that is when it puts the
underside of a beam or the inside face of a frame member in tension. Member end moments in the
slope-deflection work of Question 5 are clockwise-positive on the member, which is the usual
convention for that method. Truss forces are quoted as tension or compression rather than by
sign. Reactions are drawn in blue and applied loads in red on every figure.
A note on reading this paper. The figures are hand drawn and carry no dimensions that are not on the drawings, so the geometry of every structure below was read from the support symbols one at a time. Two readings materially affect the answers and are flagged
where they arise: the plane on which the roller of Question 2(c) bears, and the position of
the 50 kN load in Question 8.
Question 8: Reactions and internal-force diagrams for a determinate portal frame with an internal hinge (20 marks)
20 kN/m acting horizontally to the left on member 3–4, per metre of its 6 m vertical projection
Sloping legs
Both 4.5 m by 6 m, so 7.5 m long with cosines 0.6 and 0.8
Find. The four reaction components, then the shear force and bending moment diagrams for each of the three members with their maximum and minimum ordinates.
The frame: pinned at joints 1 and 4, hinged at joint 2, rigid at joint 3, with the 20 kN/m specified per metre of vertical projection.
Shear force (kN, left) and bending moment (kN·m, right) plotted normal to each member; member 1–2 carries neither.
Approach. Four reaction components need four equations, so use the three global ones plus the condition that the moment about the hinge at joint 2 vanishes for the part on either side of it. Then walk the internal actions member by member.
Confirm determinacy. Three members, four joints, four reaction
components and one internal hinge give
$$i = 3m + r - 3j - c = 9 + 4 - 12 - 1 = 0$$
so the frame is determinate, and the hinge is exactly what makes the second pin
admissible.
Resolve the distributed load. The 20 kN/m acts per metre of
vertical projection over the full 6 m height of member 3–4, so its resultant is
$$W = 20\,(6) = 120\ \text{kN}\ \text{to the left, acting at mid-height}, \; y = 3\ \text{m}$$
Because the force is purely horizontal, only its height matters when moments are taken; its
horizontal position is irrelevant.
Take global moments about joint 1. Counting anticlockwise as
positive, the 50 kN load at $(6.5,\,6)$ gives $-325$ kN·m, the 120 kN horizontal
resultant at $y = 3$ gives $+360$ kN·m, and the vertical reaction at joint 4 acts
12.5 m away:
$$-325 + 360 + 12.5\,V_{4} = 0 \;\Rightarrow\; V_{4} = \boxed{2.8\ \text{kN}\ \text{downward}}$$
$$V_{1} = 50 + 2.8 = \boxed{52.8\ \text{kN}\ \text{upward}}$$
A downward reaction at joint 4 is the frame resisting the overturning couple of the horizontal
load.
Use the hinge for the horizontal split. Member 1–2 carries no
load along its length and is attached by a pin at each end, so it is a two-force member and
its end forces must lie along it. Equivalently, take moments about joint 2 for the left part:
$$6H_{1} - 4.5V_{1} = 0 \;\Rightarrow\;
H_{1} = \tfrac{4.5}{6}\,(52.8) = \boxed{39.6\ \text{kN}\ \text{to the right}}$$
$$H_{4} = 120 - 39.6 = \boxed{80.4\ \text{kN}\ \text{to the right}}$$
Both reactions push to the right because the applied distributed load pushes the frame to the
left.
Member 1–2 — a strut with no shear and no moment. The
resultant at joint 1 is $\sqrt{39.6^{2} + 52.8^{2}} = 66.0$ kN, and its direction cosines
$39.6/66 = 0.6$ and $52.8/66 = 0.8$ are exactly those of the member, so the resultant lies
along the member axis:
$$\begin{aligned} N_{1\text{-}2} &= \boxed{66.0\ \text{kN compression}} \\ V &= 0 \\ M &= 0 \end{aligned}$$
This is the standard consequence of a member that is pinned at both ends and unloaded between
them, and it is worth spotting before any arithmetic, because it settles a whole third of the
frame at once.
Member 2–3 — shear and moment. The hinge delivers
39.6 kN horizontally and 52.8 kN vertically to joint 2, so the horizontal member carries a
constant axial compression of 39.6 kN and a shear of $+52.8$ kN over its first 2.0 m, dropping
to $+2.8$ kN beyond the 50 kN load. The moment starts at zero because joint 2 is a hinge and
builds up:
$$\begin{aligned} M_{\text{load}} &= 52.8\,(2.0) = \boxed{+105.6\ \text{kN}\cdot\text{m}} \\ M_{3} &= 105.6 + 2.8\,(1.5) = \boxed{+109.8\ \text{kN}\cdot\text{m}} \end{aligned}$$
Member 3–4 — write the moment as a function of height.
Measuring $y$ upward from joint 4 and taking the free body below the section, the reaction
components act at $y = 0$ while the accumulated distributed load $20y$ acts at $y/2$:
$$M(y) = 80.4y - 2.1y - 10y^{2} = 78.3y - 10y^{2}$$
in which the $2.1y$ term is the moment of the 2.8 kN downward reaction about the section,
whose horizontal offset is $0.75y$. Checking the ends, $M(0) = 0$ at the pin and
$M(6) = 469.8 - 360 = 109.8$ kN·m at joint 3, which matches the value carried round
from member 2–3 and confirms that joint 3 is in moment equilibrium.
Member 3–4 — extreme ordinates. Differentiating,
the moment is stationary where $78.3 - 20y = 0$, that is at $y = 3.915$ m above joint 4, and
$$M_{\max} = 78.3\,(3.915) - 10\,(3.915)^{2} = \boxed{+153.3\ \text{kN}\cdot\text{m}}$$
which is the largest moment anywhere in the frame. The shear measured perpendicular to the
member is the slope of the moment with respect to arc length, so
$$\begin{aligned} V(y) &= \frac{78.3 - 20y}{1.25} \\ V(0) &= 62.64\ \text{kN} \\ V(6) &= -33.36\ \text{kN} \end{aligned}$$
and it changes sign at the same height, 3.915 m.
Collect the diagram ordinates. On member 1–2 both diagrams
are flat at zero. On member 2–3 the shear steps from $+52.8$ kN to $+2.8$ kN and the
moment rises from zero to $+109.8$ kN·m. On member 3–4 the shear runs from
$+62.64$ kN at the pin through zero at 3.915 m to $-33.36$ kN at joint 3, and the moment rises
from zero to a maximum of $+153.3$ kN·m and falls back to $+109.8$ kN·m. Every
moment in this frame puts the inner face of the members in tension (the underside of member 2–3 and the inside face of member 3–4, which the inward 20 kN/m load bows towards the frame), so there is no sign
reversal to plot and the minimum ordinate on each member is the zero at its pinned or hinged
end.
Quantity
Value
Reaction at joint 1
39.6 kN to the right and 52.8 kN upward
Reaction at joint 4
80.4 kN to the right and 2.8 kN downward
Member 1–2
Two-force strut: 66.0 kN compression, V = 0, M = 0
Member 2–3, max shear
+52.8 kN (min +2.8 kN)
Member 2–3, max moment
+109.8 kN·m at joint 3 (min 0 at the hinge)
Member 3–4, max shear
+62.64 kN at joint 4 (min −33.36 kN at joint 3)
Member 3–4, max moment
+153.3 kN·m at 3.915 m above joint 4 (min 0 at the pin)
Check: the 50 kN load has been placed 1.5 m from joint 3, which is how the dimension line reads on the paper (its arrows close on joint 3, not on joint 2). Placing it 1.5 m from joint 2 instead moves the load to x = 6.0 m and changes the vertical reaction at joint 4 from 2.8 kN down to 4.8 kN down; state which reading you adopt.