Previous year question hub

Strength of materials - Structures - Aerospace Engineering Previous Year Questions

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

20Papers

20Years

110Questions

1Topics

Strength of materials question pattern

Every graph below is calculated only from this selection.

Questions by year

Compare question counts across years.

Difficulty distribution

How the classified questions are distributed by difficulty.

110questions

Medium 59 53.6%

Easy 49 44.5%

Hard 2 1.8%

Question type distribution

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

110questions

MCQ 56 50.9%

Numerical Answer Type (NAT) 44 40%

MSQ 9 8.2%

Fill in the blanks 1 0.9%

Subject weightage

Top subjects by unique question coverage.

Aerospace Engineering

110 Qs

Most asked topics

Top topics across the included previous year papers.

Structures

110 Qs

Subtopic coverage

Top subtopics inside this exact selection.

Strength of materials

110 Qs

Paper coverage

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

Aerospace Engineering (AE) 2026

7 Qs

Aerospace Engineering (AE) 2025

11 Qs

Aerospace Engineering (AE) 2024

8 Qs

Aerospace Engineering (AE) 2023

6 Qs

Aerospace Engineering (AE) 2022

11 Qs

Aerospace Engineering (AE) 2021

4 Qs

Aerospace Engineering (AE) 2020

10 Qs

Aerospace Engineering (AE) 2019

2 Qs

Aerospace Engineering (AE) 2018

6 Qs

Aerospace Engineering (AE) 2017

7 Qs

Aerospace Engineering (AE) 2016

9 Qs

Aerospace Engineering (AE) 2015

2 Qs

Aerospace Engineering (AE) 2014

6 Qs

Aerospace Engineering (AE) 2013

6 Qs

Aerospace Engineering (AE) 2012

5 Qs

Aerospace Engineering (AE) 2011

2 Qs

Aerospace Engineering (AE) 2010

3 Qs

Aerospace Engineering (AE) 2009

1 Qs

Aerospace Engineering (AE) 2008

1 Qs

Aerospace Engineering (AE) 2007

3 Qs

Included previous year papers

Newest papers appear first. Search these papers or sort by year and name.

Paper name	Year	PDF
Aerospace Engineering (AE) 20262026 7 questions in this view	2026	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download Official answer keyOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20252025 11 questions in this view	2025	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download Official answer keyOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20242024 8 questions in this view	2024	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download Official answer keyOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20232023 6 questions in this view	2023	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download Official answer keyOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20222022 11 questions in this view	2022	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download Official answer keyOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20212021 4 questions in this view	2021	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download Official answer keyOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20202020 10 questions in this view	2020	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20192019 2 questions in this view	2019	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20182018 6 questions in this view	2018	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20172017 7 questions in this view	2017	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20162016 9 questions in this view	2016	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20152015 2 questions in this view	2015	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20142014 6 questions in this view	2014	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20132013 6 questions in this view	2013	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20122012 5 questions in this view	2012	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20112011 2 questions in this view	2011	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20102010 3 questions in this view	2010	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20092009 1 questions in this view	2009	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20082008 1 questions in this view	2008	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download
Aerospace Engineering (AE) 20072007 3 questions in this view	2007	ExamElite PDFs ExamElite solutions Official documents Official question paperOriginal authority-issued PDF Official Download

All Strength of materials previous year questions

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2007 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2007

For a plane strain problem in the \( x-y \) plane, in general, the non-zero stress terms are

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2007 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2007

Total pressure at a point is defined as the pressure when the flow is brought to rest

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2007 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2007

Shown in the figure below is a model of an Euler-Bernoulli beam made up of two materials subjected to pure bending moment M. The Young's modulus of material A and B are E_A and E_B respectively. The sectional moment of area, about the neutral axis, of the cross-sectional areas made of materials A and B, are I_A and I_B respectively. The radius of curvature ρ of the flexural deflection of this composite beam to the bending moment M is then

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2008 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2008

In the absence of body moments, the symmetry of the stress tensor is derived from

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2009 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2009

A wing root cross section is idealized using lumped areas (booms) as shown below.
The wing root bending moment in steady level flight is \(M_y = 10\) N-m. If the airplane flies at a load factor \(n = 3.5\), the maximum bending stress at the root is

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2010 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2010

Isentropic efficiency \(\eta_d\) of a subsonic diffuser is defined as
(Note: 'a' represents the ambient, '2' represents the exit of the diffuser and 's' represents an isentropic process)

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2010 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2010

For a flow across an oblique shock which of the following statements is true?

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2010 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2010

What is the stagnation pressure at the inlet of the nozzle?

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2011 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2011

Consider the inviscid, adiabatic flow of air at free stream conditions, \( M_1 = 2 \), \( p_1 = 1 \) atm and \( T_1 = 288 \) K around a sharp expansion corner (\( \theta = 20^\circ \)) as shown below. The Prandtl-Meyer function, \( \nu \), is given as a function of Mach number, M, as \( \nu(M) = \sqrt{\frac{\gamma+1}{\gamma-1}} \tan^{-1} \sqrt{\frac{\gamma-1}{\gamma+1}(M^2-1)} - \tan^{-1} \sqrt{M^2-1} \). Assume air to be calorically perfect with \( \gamma = 1.4 \). The Mach number, \( M_2 \), downstream of the expansion corner is approximately

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2011 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2011

The shock angle \( \beta \) is

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2012 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2012

The critical Mach number of an airfoil is attained when

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2012 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2012

The shadowgraph flow visualization technique depends on

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2012 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2012

The Mach angle for a flow at Mach 2.0 is

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2012 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2012

The ideal static pressure coefficient of a diffuser with an area ratio of 2.0 is

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2012 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2012

In a closed-circuit supersonic wind tunnel, the convergent-divergent (C-D) nozzle and test section are followed by a C-D diffuser to swallow the starting shock. Here, we should have the

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2014 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2014

For inviscid, supersonic flow over a diamond shaped airfoil, shown in the figure, which statement is correct among the following?

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2014 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2014

Consider supersonic flow near a corner (at an angle \( \theta \) from the horizontal) with an attached oblique shock (at an angle \( \beta \) with horizontal) as shown in figure. If Mach number \( M \) decreases gradually from a high supersonic value, which of the following statements is correct?

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2014 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2014

A student needs to find velocity across a stationary normal shock. He measures density and pressure across the shock as shown in the figure below. \(1\ bar = 10^5 Pa\). (No shock table is needed for the calculations). The value of \(u_1\) in m/s is ______.

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2014 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2014

For inviscid, compressible flow past a thin airfoil, shown in the figure, free-stream Mach number and pressure are denoted by \(M_\infty\) and \(p_\infty\) respectively. Ratio of pressure at point A and \(p_\infty\) is 0.8 and specific heat ratio is 1.4. If the Mach number at point A is 1.0 and rest of the flow field is subsonic, the value of \(M_\infty\) is

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2014 · Aerospace Engineering · Structures · Strength of materials

Aerospace Engineering (AE) 2014

A cruise missile with an ideal ramjet engine is flying at Mach 4.0 at an altitude where the ambient temperature is 100K. Consider ratio of specific heats γ = 1.4 and specific gas constant R = 287 J/kgK. If the stagnation temperature in the combustion chamber is equal to 2310K, the speed of the exhaust gases (in m/s) is ______.

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Strength of materials - Structures - Aerospace Engineering Previous Year Questions