Aerospace Engineering Gate 2010 Questions with Answer

Ques 53 GATE 2010


In a general case of a homogeneous material under thermo-mechanical loading the number of
distinct components of the state of stress is

A

3

B

4

C

5

D

6


(d) is the correct answer.

Ques 54 GATE 2010


A vertical slender rod is suspended by a hinge at the top and hangs freely. It is heated until it attains
a uniform temperature, 7. Neglecting the effect of gravity, the rod has

A

Stress but no strain

B

Strain but no stress

C

Both stress and strain

D

Neither stress nor strain


(b) is the correct answer.

Ques 55 GATE 2010


A thin rectangular plate made of isotropic material which satisfies the octahedral (i.e., Von Mises/
Distortion energy) failure criterion has yield strength of 200 MPa under uniaxial tension. As shown
in the figure, if it is loaded with uniform tension of 150 MPa along the x-direction, the maximum
uniform tensile stress that can be applied along the y-direction before the plate starts yielding is
about

A

227 MPa

B

77 MPa

C

87 MPa

D

114 MPa


(a) is the correct answer.

Ques 56 GATE 2010


A column of length I and flexural rigidity El, has one end fixed and the other end hinged. The
critical buckling load for the column is

A

π2EI/(0.5l)2

B

π2EI/(0.7i)2

C

π2EI/t2

D

π2EI/(2l)2


(b) is the correct answer.

Ques 57 GATE 2010


A horizontal cantilevered steel beam of rectangular cross-section having width b and depth d is
vibrating in the vertical plane. The natural frequency of bending vibration is highest when

A

b=10, d=10

B

b=20, d=5

C

b=5, d=20

D

b=25, d=4


(c) is the correct answer.

Ques 58 GATE 2010


Following stress state is proposed for a 2-D problem with no body forces: σxx=3x2y+4y2.
σyy=y3+14xy τxy=-3xy2-7x2 It satisfies

A

Equilibrium equations but not compatibility equation

B

Compatibility equation but not equilibrium equations

C

Neither equilibrium equations nor compatibility equation

D

Both equilibrium equations and compatibility equation


(a) is the correct answer.

Ques 59 GATE 2010


The thin rectangular plate shown in the figure is loaded with uniform shear,
τ0 along all edges and
uniform uniaxial tension in the y-direction. The appropriate Airy's stress function to solve for
stresses is given by

A

axy-σ_x22_(x4-y4)

B

τoxy-σox22

C

oxy+σox22

D

τoxy+σox22o(x4-y4)


(c) is the correct answer.

Ques 60 GATE 2010


The given thin wall section of uniform thickness, s, is symmetric about x-axis. Moment of inertia is
given to be Ixx=3512th3.
Shear center for this section is located at

A

x=-3/8h

B

x=-9/28h

C

x=-35/36h

D

x=-17/35h


(b) is the correct answer.

Ques 61 GATE 2010


Consider a simply supported beam of length L, carrying a bracket welded at its center. The bracket carries a vertical load, P, as shown in the figure. Dimensions of bracket are a = 0.1L. The beam has a square cross section of dimension h × h.

Bending moment diagram is given by

A

B

C

D


(a) is the correct answer.

Ques 62 GATE 2010


Consider a simply supported beam of length L, carrying a bracket welded at its center. The bracket carries a vertical load, P, as shown in the figure. Dimensions of bracket are a = 0.1L. The beam has a square cross section of dimension h × h.

Maximum value of shear stress is

A

0.67 P/h2

B

1.33 P/h2

C

1.5 P/h2

D

0.9 P/h2


(c) is the correct answer.

Ques 63 GATE 2010


A spacecraft of mass 100 kg. moving at an instantaneous speed of 1.8×104m/s, picks up
interstellar dust at the rate of 3.2×10-8kg/s. Assuming that the dust was initially at rest, the
instantaneous rate of retardation of the spacecraft is:


(5.76×10-6) is the correct answer.

Ques 64 GATE 2010


A uniform cross-section rigid rod of mass m and length , is hinged at its upper end and suspended
like a pendulum. Its natural frequency for small oscillations is

A

g/2l

B

g/l

C

2g/l

D

3g/2l


(d) is the correct answer.

Ques 65 GATE 2010


During an under-damped oscillation of a single degree of freedom system, in the time-displacement
plot the third peak is of magnitude 100 and the tenth peak is of magnitude 10. The damping ratio ζ
is approximately:

A

0.052

B

0.023

C

0.366

D

0.159


(a) is the correct answer.

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