Aerospace Engineering GATE 2011 Questions with Answer

Ques 1 Aerodynamics


It is seen that the drag polar of a certain aerofoil is symmetric about the Cd axis. This drag polar
could refer to

A

NACA 0012

B

NACA 4415

C

NACA 23012

D

None of the above


Ques 2 Aerodynamics


The aerodynamic centre of a supersonic aerofoil, with chord c, is located at

A

the leading edge

B

0.25c

C

0.5c

D

0.75c


Ques 3 Aerodynamics


Winglets are used on wings to minimize

A

skin friction drag

B

profile drag

C

wave drag

D

induced drag


Ques 4 Aerodynamics


In the context of Prandtl's lifting line theory for a finite wing, which of the following combinations
of statements is TRUE?
P: The bound vortex is responsible for the lift force
Q: The trailing vortices are responsible for the induced drag
R: The bound vortex is responsible for the induced drag
S: The trailing vortices are responsible for the lift force

A

P,Q

B

Q,R

C

R,S

D

P,S


Ques 5 Aerodynamics


Consider flow over a thin aerofoil at Mach number, Mx=0.5 at an angle of attack, a. Using the Prandtl-Glauert rule for compressibility correction, the formula for lift coefficient, cb can be written as

A

5.44α

B

6.28α

C

7.26α

D

14.52α


Ques 6 Aerodynamics


Prandtl’s lifting line equation for a general wing is given by where U is the free-stream velocity, α is the angle of attack, y0 is the spanwise location, αL=0(y0) gives the spanwise variation of zero-lift angle, c is the chord, b is the span, and Γ(y0) gives the spanwise variation of circulation.
The rate of change of circulation with angle of attack Γα=∂Γ/∂α is

A

inversely proportional to α

B

independent of α

C

a linear function of α

D

a quadratic function of α


Ques 7 Aerodynamics


Prandtl’s lifting line equation for a general wing is given by where U is the free-stream velocity, α is the angle of attack, y0 is the spanwise location, αL=0(y0) gives the spanwise variation of zero-lift angle, c is the chord, b is the span, and Γ(y0) gives the spanwise variation of circulation.
Given that , the corresponding lift curve-slope is
∂CL/∂α is

A

independent of α

B

a linear function of α

C

a quadratic function of α

D

a cubic function of α


Ques 8 Engineering Mathematics


Consider x, y, z to be right-handed Cartesian coordinates. A vector function is defined in this
coordinate system as v=3xi+3xyj-yz2k, where i, j and k are the unit vectors along x, y and
z axes, respectively. The curl of v is given by

A

z2i-3yk

B

z2j+3yk

C

z2i+3yj

D

-z2i+3yk


Ques 9 Engineering Mathematics


Which of the following functions is periodic?

A

f(x)=x2

B

f(x)=log x

C

f(x)=ex

D

f(x)=const


Ques 10 Engineering Mathematics


The function
f(x1,x2,x3)=x12+x22+x32-2x1-4x2-6x3+14 has its minimum value at

A

(1, 2, 3)

B

(0, 0, 0)

C

(3, 2, 1)

D

(1, 1, 3)


Ques 11 Engineering Mathematics


Consider the function f(x1,x2)=x12+2x22+e-x1-x2 The vector pointing in the direction of
maximum increase of the function at the point (1, -1) is

A

B

C

D


Ques 12 Engineering Mathematics


Two simultaneous equations given by y=π+x and y=x-π have

A

a unique solution

B

infinitely many solutions

C

no solution

D

a finite number of multiple solutions


Ques 13 Engineering Mathematics


Consider the function f(x)=x-sin(x). The Newton-Raphson iteration formula to find the root of
the function starting from an initial guess x(0) at iteration k is

A

x(k+1)=sin x(k)-x(k)cos xk/1-cos x(k)

B

x(k+1)=sin x(k)-x(k)cos xk/1+cos x(k)

C

x(k+1)=sin x(k)+x(k)cos xk/1-cos x(k)

D

x(k+1)=sin x(k)+x(k)cos xk/1+cos x(k)


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