Trusses


Question 1
An idealised bridge truss is shown in the figure. The force in Member U_{2} L_{3} is _____ kN (round off to one decimal place).

A
12.5
B
16.8
C
14.1
D
10.6
GATE CE 2023 SET-1   Structural Analysis
Question 1 Explanation: 


\sum F_{y}=0, \quad 50-20-20-F_{U_{2} L_{3}} \sin 45^{\circ}=0
\therefore \quad F_{U_{2} L_{3}}=\frac{10}{\sin 45^{\circ}}=14.14 \mathrm{kN}
\therefore Rounding off to one decimal.
Question 2
Consider the pin-jointed truss shown in the figure (not to scale). All members have the same axial rigidity, \mathrm{AE}. Members \mathrm{QR}, \mathrm{RS}, and \mathrm{ST} have the same length L. Angles OBT, RCT, SDT are all 90^{\circ}. Angles BQT, CRT, DST are all 30^{\circ}. The joint T carries a vertical load P. The vertical deflection of joint T is k \frac{P L}{A E}. What is the value of k ?

A
1.5
B
4.5
C
3
D
9
GATE CE 2023 SET-1   Structural Analysis
Question 2 Explanation: 


Considering joint T,

\sum F_{y}=0, \quad F_{Q T} \sin 60^{\circ}=P
\therefore \quad \mathrm{F}_{\mathrm{QT}}=\frac{2 \mathrm{P}}{\sqrt{3}}
\sum \mathrm{F}_{\mathrm{X}}=0, \mathrm{~F}_{\mathrm{BT}}=-\mathrm{F}_{\mathrm{QT}} \cos 60^{\circ}=-\frac{P}{\sqrt{3}}
\therefore \quad Strain energy (U)=\left(\frac{P^{2} L}{2 A E}\right)_{Q T}+\left(\frac{P^{2} L}{2 A E}\right)_{B T}
=\frac{\left(\frac{2 \mathrm{P}}{\sqrt{3}}\right)^{2}(3 \mathrm{~L})}{2 \mathrm{AE}}+\frac{\left(-\frac{\mathrm{P}}{\sqrt{3}}\right)^{2}\left(\frac{3 \mathrm{~L}}{2}\right)}{2 \mathrm{AE}}
=\frac{2 P^{2} \times L}{A E}+\frac{P^{2} \times L}{4 A E}
\frac{8 P^{2} L+P^{2} L}{4 A E}=\frac{9 P^{2} L}{4 A E}
\therefore \quad Vertical deflection of joint T
=\frac{\partial \mathrm{U}}{\partial \mathrm{P}}=\frac{18 \mathrm{PL}}{4 \mathrm{AE}}=4.5 \frac{\mathrm{PL}}{\mathrm{AE}}
\therefore \quad \mathrm{K}=4.5


Question 3
The plane truss shown in the figure is subjected to an external force P. It is given that P = 70 kN, a = 2 m, and b = 3 m.

The magnitude (absolute value) of force (in kN) in member EF is _______. (round off to the nearest integer)
A
12
B
30
C
87
D
92
GATE CE 2022 SET-1   Structural Analysis
Question 3 Explanation: 


\begin{aligned} \Sigma M_J&=0\\ V_A \times 8-H_A \times 1-70 \times 4&=0\\ 8V_A-H_A&=280 \;\;\;(i) \end{aligned}
To find H_A (Cut the truss by 1-1)
Consider left hand side
\begin{aligned} \Sigma M_E&=0\\ V_A \times 4-H_A \times 4&=0\\ V_A&=H_A \;\;\;(ii)\\ \text{using (i) and (ii)}&\\ 8V_A-V_A&=280\\ 7V_A&=280\\ V_A&=40kN\\ H_A&=40kN\\ H_J&=40kN\\ V_J&=70-40=30kN\\ \end{aligned}
To find force in member EF (Cit the truss by 2-2)
Consider right hand side
Force in member EF
F_{EF}=V_J=30kN
Question 4
Refer the truss as shown in the figure (not to scale).

If load, F=10 \sqrt{3} \mathrm{kN}, moment of inertia, I=8.33 \times 10^{6} \mathrm{~mm}^{4}, area of cross-section, A=10^{4} \mathrm{~mm}^{2}, and length, L=2 m for all the members of the truss, the compressive stress (in \mathrm{kN} / \mathrm{m}^{2},in integer) carried by the member Q-R is _________
A
370
B
650
C
760
D
500
GATE CE 2021 SET-1   Structural Analysis
Question 4 Explanation: 


V_{P}=V_{S}=5 \sqrt{3} \mathrm{kN}
Considering equilibrium of LHS of section (1 )-(1)


Taking moment about 'T'
\begin{aligned} \Sigma M_{T}(C W)&=0\\ (5 \sqrt{3} \times a)+F_{Q R}\left(\frac{\sqrt{3} a}{2}\right)&=0\\ \Rightarrow \qquad \qquad \qquad \qquad \quad F_{O A}&=-10 \mathrm{kN} or 10 \mathrm{kN} (C) \\ \text{ Compressive} &\text{ stress in member QR} \left(\sigma_{\mathrm{C}}\right)\\ \sigma_{\mathrm{C}}&=\frac{F_{Q A}}{2 A} \\ &=\frac{10 \mathrm{kN}}{2 \times\left(10^{4} \times 10^{-6}\right) \mathrm{m}^{2}} \\ &=500 \mathrm{kN} / \mathrm{m}^{2} \end{aligned}
Question 5
A truss EFGH is shown in the figure, in which all the members have the same axial rigidity R. In the figure, P is the magnitude of external horizontal forces acting at joints F and G.

If R=500 \times 10^{3} \mathrm{kN},P=150 \mathrm{kN} and L=3 m, the magnitude of the horizontal displacement of joint G (in mm,round off to one decimal place) is ________
A
0.4
B
0.6
C
0.9
D
0.2
GATE CE 2021 SET-1   Structural Analysis
Question 5 Explanation: 




Note: No need to calculate 'I< force in all members because 'P force is zero fore all members except FG
By unit load method
\begin{aligned} \text { 1. } \Delta_{\mathrm{HG}}=& \sum_{i=1}^{n} \frac{P_{i} k_{i} L_{i}}{A_{i} E_{i}} \\ \Delta_{\mathrm{HG}}=& \text { Horizontal deflection at joint } \mathrm{G} \\ \therefore \qquad & \qquad \qquad\Delta_{\mathrm{HG}} =\underbrace{\frac{P \times 1 \times L}{A E}}_{\text {FG-member }} \times \underbrace{Q^{\prime}}_{\text {(For all other members) }} \\ & \qquad \qquad\Delta_{\mathrm{HG}} =\frac{P L}{A E}=\left(\frac{150 \times 3}{500 \times 10^{3}} \times 10^{3}\right) \mathrm{mm} \\ & \qquad \qquad \qquad=0.90 \mathrm{~mm} \end{aligned}


There are 5 questions to complete.

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