Aircraft Force Systems Online Exam Quiz
Aircraft Force Systems GK Quiz. Question and Answers related to Aircraft Force Systems. MCQ (Multiple Choice Questions with answers about Aircraft Force Systems
Air data computer system measures airspeed, mach number, temperature and height.
Options
A : TRUE
B : FALSE
C : -
D : -
Below the mach number 0.5 the flow is considered as incompressible flow.
Options
A : TRUE
B : FALSE
C : -
D : -
Dynamic pressure is the difference between stagnation pressure and static pressure.
Options
A : TRUE
B : FALSE
C : -
D : -
FSO stands for __
Options
A : Full-scale output
B : Flight-scale output
C : Flight stimulation output
D : Full screen output
In transonic region the mach number affects the aerodynamic characteristics.
Options
A : TRUE
B : FALSE
C : -
D : -
The range of Re in the typical flight is ___
Options
A : 106 to 109
B : 105 to 109
C : 106 to 108
D : 106 to 1010
Transducers are the pressure devices used to convert signal in one form of energy to another energy form.
Options
A : TRUE
B : FALSE
C : -
D : -
What is the critical mach number for most subsonic aircraft?
Options
A : Around 0.8
B : Around 2
C : Around 1
D : Around 1.5
What is the range of mach number for a conventional aircraft?
Options
A : 0 to 3.2
B : 0 to 2.2
C : 0 to 4.2
D : 0 to 1.2
Which of the following are the forces that are concerned with the performance of an aircraft?
Options
A : Lift, drag, weight
B : Lift, drag, side force
C : Lift, drag
D : Lift, drag, weight, side force
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