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Laminar Flow in Aerodynamics
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Pitot_tube_with_flat_faces_are_more_sensitive.$..
1.
Pitot_tube_with_flat_faces_are_more_sensitive.$
A.
True
B.
False
Answer» C.
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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.
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