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Previous year question hub

Propulsion - Aerospace Engineering Previous Year Questions

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

20Papers
20Years
218Questions
1Topics

Propulsion 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.

Medium 106 48.6%
Easy 105 48.2%
Hard 7 3.2%

Question type distribution

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

MCQ 141 64.7%
Numerical Answer Type (NAT) 65 29.8%
MSQ 9 4.1%
Fill in the blanks 3 1.4%

Subject weightage

Top subjects by unique question coverage.

Aerospace Engineering
218 Qs

Most asked topics

Top topics across the included previous year papers.

Propulsion
218 Qs

Subtopic coverage

Top subtopics inside this exact selection.

Rockets
97 Qs
Turbomachinery
68 Qs
Gas turbine combustor
43 Qs
Propulsion Thermodynamics and Brayton Cycle
5 Qs
Air Intakes and Nozzles
3 Qs
Aircraft Engine Performance
2 Qs

Paper coverage

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

Aerospace Engineering (AE) 2026
17 Qs
Aerospace Engineering (AE) 2025
9 Qs
Aerospace Engineering (AE) 2024
10 Qs
Aerospace Engineering (AE) 2023
12 Qs
Aerospace Engineering (AE) 2022
8 Qs
Aerospace Engineering (AE) 2021
11 Qs
Aerospace Engineering (AE) 2020
9 Qs
Aerospace Engineering (AE) 2019
9 Qs
Aerospace Engineering (AE) 2018
11 Qs
Aerospace Engineering (AE) 2017
11 Qs
Aerospace Engineering (AE) 2016
12 Qs
Aerospace Engineering (AE) 2015
4 Qs
Aerospace Engineering (AE) 2014
11 Qs
Aerospace Engineering (AE) 2013
12 Qs
Aerospace Engineering (AE) 2012
12 Qs
Aerospace Engineering (AE) 2011
10 Qs
Aerospace Engineering (AE) 2010
9 Qs
Aerospace Engineering (AE) 2009
12 Qs
Aerospace Engineering (AE) 2008
14 Qs
Aerospace Engineering (AE) 2007
15 Qs

Browse by subtopics

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

Included previous year papers

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

Paper nameYearPDFAttempt
Aerospace Engineering (AE) 20262026
17 questions in this view
2026
Aerospace Engineering (AE) 20252025
9 questions in this view
2025
Aerospace Engineering (AE) 20242024
10 questions in this view
2024
Aerospace Engineering (AE) 20232023
12 questions in this view
2023
Aerospace Engineering (AE) 20222022
8 questions in this view
2022
Aerospace Engineering (AE) 20212021
11 questions in this view
2021
Aerospace Engineering (AE) 20202020
9 questions in this view
2020
Aerospace Engineering (AE) 20192019
9 questions in this view
2019
Aerospace Engineering (AE) 20182018
11 questions in this view
2018
Aerospace Engineering (AE) 20172017
11 questions in this view
2017
Aerospace Engineering (AE) 20162016
12 questions in this view
2016
Aerospace Engineering (AE) 20152015
4 questions in this view
2015
Aerospace Engineering (AE) 20142014
11 questions in this view
2014
Aerospace Engineering (AE) 20132013
12 questions in this view
2013
Aerospace Engineering (AE) 20122012
12 questions in this view
2012
Aerospace Engineering (AE) 20112011
10 questions in this view
2011
Aerospace Engineering (AE) 20102010
9 questions in this view
2010
Aerospace Engineering (AE) 20092009
12 questions in this view
2009
Aerospace Engineering (AE) 20082008
14 questions in this view
2008
Aerospace Engineering (AE) 20072007
15 questions in this view
2007

Sample previous year questions

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

1
2007 · Aerospace Engineering · Propulsion · Turbomachinery
Aerospace Engineering (AE) 2007
Which one of the following engines should be used by a subsonic passenger transport airplane for minimum specific fuel consumption?
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2
2008 · Aerospace Engineering · Propulsion · Rockets
Aerospace Engineering (AE) 2008
The degree of reaction of an impulse turbine is
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3
2009 · Aerospace Engineering · Propulsion · Turbomachinery
Aerospace Engineering (AE) 2009
The propulsive efficiency of a turbo-jet engine moving at velocity \(U_{\infty}\) and having exhaust velocity \(U_e\) with respect to the engine is given by
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4
2010 · Aerospace Engineering · Propulsion · Rockets
Aerospace Engineering (AE) 2010

For a multi-stage axial compressor with constant diameter hub

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5
2011 · Aerospace Engineering · Propulsion · Gas turbine combustor
Aerospace Engineering (AE) 2011
Consider a single degree of freedom spring-mass-damper system with mass, damping and stiffness of \(m\), \(c\) and \(k\), respectively. The logarithmic decrement of this system can be calculated using
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6
2012 · Aerospace Engineering · Propulsion · Rockets
Aerospace Engineering (AE) 2012

The ratio of flight speed to the exhaust velocity for maximum propulsion efficiency is

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