The dynamic pressure can be used in all flows from incompressible to h – McqOptions

MCQOPTIONS

1.	The dynamic pressure can be used in all flows from incompressible to hypersonic.
A.	True
B.	False
Answer» B. False

Discussion

No Comment Found

Related MCQs

The lower end of the pitot tube is bet at an angle of ____________
In a pitot tube, the kinetic energy is converted into _________
Pitot tube with flat faces are more sensitive.
An aircraft is flying at cruise level with a velocity of 110m/s at an altitude of 10 km and the dynamic pressure is 5.43kN/m2. Now assume the aircraft is flying is at sea level with a speed of 65m/s and the same dynamic pressure. In the above data, the velocity 65m/s refers to __________
When the local flow velocity is zero itself then _________
AN_AIRCRAFT_IS_FLYING_AT_CRUISE_LEVEL_WITH_A_VELOCITY_OF_110M/S_AT_AN_ALTITUDE_OF_10_KM_AND_THE_DYNAMIC_PRESSURE_IS_5.43KN/M<SUP>2</SUP>._NOW_ASSUME_THE_AIRCRAFT_IS_FLYING_IS_AT_SEA_LEVEL_WITH_A_SPEED_OF_65M/S_AND_THE_SAME_DYNAMIC_PRESSURE._IN_THE_ABOVE_DATA,_THE_VELOCITY_65M/S_REFERS_TO___________?$
In a pitot tube, the kinetic energy is converted into _________$
Pitot_tube_with_flat_faces_are_more_sensitive.$
The pressure measured relative to vacuum is ______
When an aircraft is grounded, the pitot static tube is generally covered.