- Total number of questions: 65
- 30 questions carry one mark each
- 35 questions carry two marks each
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Exam Details
Aerospace Engineering (AE) 2010
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Questions
65
Duration
180 mins
Package
Aerospace Engineering (AE) - Previous Year Papers
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Instructions
Aerospace Engineering (AE) 2010 – Instructions
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Sample questions from this paper
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2010 · Unclassified
Aerospace Engineering (AE) 2010
Q.1 – Q.25 carry one mark each.
Isentropic efficiency η0 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)
2010 · Unclassified
Aerospace Engineering (AE) 2010
Two position vectors are indicated by V̅1 = [x1 y1] and V̅2 = [x2 y2]. If a2 + b2 = 1, then the operation V̅'2 = [a -b b a] V̅2 amounts to obtaining the position vector V̅'2 from V̅1 by
2010 · Unclassified
Aerospace Engineering (AE) 2010
An aircraft is climbing at a constant speed in a straight line at a steep angle of climb. The load factor it sustains during the climb is:
2010 · Unclassified
Aerospace Engineering (AE) 2010
In a general case of a homogeneous material under thermo-mechanical loading the number of distinct components of the state of stress is
2010 · Unclassified
Aerospace Engineering (AE) 2010
The linear second order partial differential equation ∂2φ/∂x2 + ∂2φ/∂xy + ∂2φ/∂y2 + 9φ = 0 is
2010 · Unclassified
Aerospace Engineering (AE) 2010
All other factors remaining constant, if the weight of an aircraft increases by 30% then the takeoff distance increases by approximately: