My Cart
Your Cart 0

    Your cart is empty.

  • Total (Amount) ₹0.00
Exam Details

Aerospace Engineering (AE) 2017

Review the key details, then start the test when you are ready. You can also open the full package to see related papers.

Questions 65
Duration 180 mins
Package Aerospace Engineering (AE) - Previous Year Papers

Paper pattern & analysis

Filter this paper by subject, topic or subtopic. Every graph updates from the selected questions.

Explore previous papers
Showing all 65 questions in this paper.

Subject distribution

No subject classification is available.

Topic distribution

No topic classification is available.

Subtopic distribution

No subtopic classification is available.

Difficulty distribution

Easy 36 55.4%
Hard 29 44.6%

Question type distribution

Multiple Choices 36 55.4%
Fill in the blanks 29 44.6%

Instructions

Aerospace Engineering (AE) 2017 – Instructions
  • Total number of questions: 65
  • 30 questions carry one mark each
  • 35 questions carry two marks each
  • Negative marking: 1/3 of the marks allotted to the question
  • Use of calculator is allowed
  • This is a proctored examination
  • All other browser applications will be automatically closed
  • After three warnings, the examination window will close automatically

Syllabus

Full Syllabus

Sample questions from this paper

Questions are selected across the paper subjects wherever the paper contains that variety.

1
2017 · Unclassified
Aerospace Engineering (AE) 2017
Q.1 – Q.5 carry one mark each.

Given the vectors v1 = i + 3j; v2 = 2i - 4j + 3k, the vector v3 that is perpendicular to both v1 and v2 is given by:

A
v₃ = v₁ - (v₁ ⋅ v₂) v₂ / |v₂|²
B
v₃ = k̂
C
v₃ = v₂ - (v₂ ⋅ v₁) v₁ / |v₁|²
D
v₃ = v₁ × v₂ / |v₁ × v₂|
2
2017 · Unclassified
Aerospace Engineering (AE) 2017

The value of the integral I = ∮C ((x - y)dx + x2dy), with C the boundary of the square 0 ≤ x ≤ 2; 0 ≤ y ≤ 2, is ________

Write your response
3
2017 · Unclassified
Aerospace Engineering (AE) 2017

Let v(t) be a unit vector that is a function of the parameter t. Then v̇ ⋅ dv/dt = ________

Write your response
4
2017 · Unclassified
Aerospace Engineering (AE) 2017

The eigenvalues λn and eigenfunctions un(x) of the Sturm-Liouville problem d2y/dx2 + k2λy = 0, 0 < x < 1; y(0) = 0, y(1) = 0 are given by:

A
λₙ = n²π²; uₙ(x) = sin λₙx, n = 0, ±1, ±2, ⋯, ∞
B
λₙ = n²π²/k²; uₙ(x) = sin knx, n = 0, ±1, ±2, ⋯, ∞
C
λₙ = n²π²/k²; uₙ(x) = sin nπx, n = 0, ±1, ±2, ⋯, ∞
D
λₙ = n²π²; uₙ(x) = sin nπx, n = 0, ±1, ±2, ⋯, ∞
5
2017 · Unclassified
Aerospace Engineering (AE) 2017
Correct : 1 Wrong : -0.33

3-point Gaussian integration formula is given by: ∫_-11 f(x)dx ≈ Σj=13 Aj f(xj) with x1 = 0, x2 = -x3 = -√(3/5); A1 = 8/9, A2 = A3 = 5/9. This formula exactly integrates

A
f(x) = 5 - x⁷
B
f(x) = 2 + 3x + 6x⁴
C
f(x) = 13 + 6x³ + x⁶
D
f(x) = e⁻x²
6
2017 · Unclassified
Aerospace Engineering (AE) 2017
Q.6 – Q.10 carry two marks each.

Which one of the following statements is NOT true

A
The pitching moment of any airfoil at any angle of attack is always zero at the center of pressure
B
The pitching moment of any airfoil at any angle of attack is always zero at the aerodynamic center
C
The center of pressure and aerodynamic center coincide for a symmetric airfoil
D
The pitching moment about the aerodynamic center, for any airfoil, does not vary with angle of attack