Question: Below the mach number 0.5 the flow is considered as incompressible flow.
Options
A : TRUE
B : FALSE
C : -
D : -
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Aircraft Force Systems more questions
The propulsive force developed by the engine-propeller combination is given....
The rate of climb is given by ___
The relative airspeed for maximum gradient of climb is a....
What is the relation between climb rate and power speed?
Air data computer system measures airspeed, mach number, temperature and....
Dynamic pressure is the difference between stagnation pressure and static....
In transonic region the mach number affects the aerodynamic characteristics.
The range of Re in the typical flight is ___
Transducers are the pressure devices used to convert signal in....
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