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Previous year question hub

Structures - Aerospace Engineering Previous Year Questions

Practice Structures - Aerospace Engineering previous year questions organised from real papers, with year-wise coverage and clear topic navigation.

2Papers
2Years
17Questions
1Topics

Structures question pattern

Every graph below is calculated only from this selection.

Questions by year

Year-wise coverage for Structures. Each bar uses a separate theme-derived color.

Difficulty distribution

How the classified questions are distributed by difficulty.

Medium 9 52.9%
Easy 8 47.1%

Question type distribution

MCQ, numerical, multiple-select and other formats found in these papers.

Numerical Answer Type (NAT) 9 52.9%
Multiple Choices 8 47.1%

Subject weightage

Top subjects by unique question coverage.

Aerospace Engineering
17 Qs

Most asked topics

Top topics across the included previous year papers.

Structures
17 Qs

Subtopic coverage

Top subtopics inside this exact selection.

Strength of materials
15 Qs
Structural Dynamics
2 Qs

Paper coverage

Question coverage for the most populated papers. Every active PYP paper remains listed below.

Aerospace Engineering (AE) 2026
5 Qs
Aerospace Engineering (AE) 2025
12 Qs

Browse by subtopics

Open a focused page built from the same verified paper data.

Strength of materials

Explore previous-paper coverage, trends and focused practice for Strength of materials.

15 questions2 papers2 years

Structural Dynamics

Explore previous-paper coverage, trends and focused practice for Structural Dynamics.

2 questions2 papers2 years

Included previous year papers

Newest papers appear first. Sort by year, question coverage or name.

PaperYear / sessionQuestions in this viewOpen
Aerospace Engineering (AE) 202620265View paper
Aerospace Engineering (AE) 2025202512View paper

Sample previous year questions

A varied preview from the papers represented in this selection, with every available option.

1
2025 · Aerospace Engineering · Structures · Strength of materials
Aerospace Engineering (AE) 2025
For a homogeneous, isotropic material, the relation between the shear modulus (\(G\)), Young's modulus (\(E\)), and Poisson's ratio (\(\nu\)) is ____.
A
\(G = 2E(1 + \nu)\)
B
\(2G = E(1 + \nu)\)
C
\(E = 2G(1 + \nu)\)
D
\(2E = G(1 + \nu)\)
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2
2026 · Aerospace Engineering · Structures · Strength of materials
Aerospace Engineering (AE) 2026
The number of independent elastic constants that a fully anisotropic linear elastic material can have is ______.
A

36

B

21

C

10

D

2

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3
2025 · Aerospace Engineering · Structures · Strength of materials
Aerospace Engineering (AE) 2025
A simply supported horizontal beam is subjected to a distributed transverse load varying linearly from \(q_0\) at A to zero at B, as shown in the figure. Which one of the following options is correct?

Question diagram

A
The magnitude of the vertical reaction force at A is larger than that at B.
B
The magnitude of the vertical reaction force at B is larger than that at A.
C
The magnitudes of the vertical reaction forces at A and B are equal.
D
The reactions at points A and B are indeterminate.
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4
2026 · Aerospace Engineering · Structures · Strength of materials
Aerospace Engineering (AE) 2026
A cantilever beam with an unsymmetric cross-section is subjected to a transverse shear force (P) at its free end. P acts at the shear center of the beam cross-section. Which one of the following statements is TRUE about the deformation of this beam?
A

The beam undergoes only torsion

B

The beam undergoes only bending

C

The beam undergoes both torsion and bending

D

The beam undergoes neither torsion nor bending

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5
2025 · Aerospace Engineering · Structures · Strength of materials
Aerospace Engineering (AE) 2025
A stress field is given by \(\sigma_{xx} = \sigma_{zz} = C_1 y\), \(\sigma_{yy} = C_2 y\), \(\tau_{xy} = \tau_{yz} = \tau_{zx} = 0\), where \(C_1\) and \(C_2\) are non-zero constants. If the stress field satisfies equilibrium, which one of the following options is correct?
A
There is no body force per unit volume.
B
There is a constant body force per unit volume in the y-direction.
C
The body force per unit volume varies linearly in the y-direction.
D
The direction of the body force per unit volume depends on the value of \(C_1\).
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6
2026 · Aerospace Engineering · Structures · Strength of materials
Aerospace Engineering (AE) 2026
A thin-walled circular tube is made of a material whose magnitude of the ultimate strength, both in tension and compression, is 200 MPa. The mean radius of the tube is 0.2 m and the wall thickness is 0.004 m. Based on the maximum stress criteria, the maximum torque that the tube can sustain is __________ kN-m (round off to the nearest integer).
Enter a numerical response
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