Explore topic-wise MCQs in Aircraft Design.

This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Design knowledge and support exam preparation. Choose a topic below to get started.

1.

Stick fixed neutral point is defined at 40% of chord. Choose appropriate location of Stick free neutral point.

A. 0.39
B. 0.8
C. 0.65
D. 0.5
Answer» B. 0.8
2.

Find the value of CHδe if tail angle of attack is 3 deg and CHɑt is -0.004. Consider elevator floats up by 2 degree.

A. -0.006
B. -7
C. 1.223
D. 1.225
Answer» B. -7
3.

Determine the value of tail angle of attack if, elevator floats down by 1.8 degree. Consider CHδe as 0.003 and CHɑt as -0.006.

A. 0.9
B. 2.5
C. 3.4
D. 1.8
Answer» B. 2.5
4.

Find the degree of elevator float. Consider tail AOA is 2° and CHδe= -0.005, CHɑt=-0.0052.

A. 2.08 deg
B. 4
C. 12
D. 2.119
Answer» B. 4
5.

Negative stick force gradient is used to provide ___________

A. speed stability
B. thrust
C. propulsive force
D. gliding ratio
Answer» B. thrust
6.

Hinge moment coefficient depends upon ________

A. Tail AOA, elevator deflection, etc
B. Only tail angle
C. Only wing angle
D. Lift to drag ratio of fuselage
Answer» B. Only tail angle
7.

Which of the following is correct for hinge moment?

A. Hinge moment coefficient is function of tail angle of attack
B. Hinge moment is not dependent on the tail angle
C. Downwash is used to reduces angle of attack at tail
D. Lifting property of the airfoil is same as a sphere
Answer» B. Hinge moment is not dependent on the tail angle
8.

Stick force is function of ___________

A. hinge moment
B. lofting
C. fuel air ratio
D. pressure ratio of inlet
Answer» B. lofting
9.

Stick fixed and stick free are similar.

A. True
B. False
Answer» C.
10.

Stick free stability permits ____________

A. elevator to float
B. elevator to be fixed
C. fixed rigid body
D. lift and drag ratio
Answer» B. elevator to be fixed