Aerospace Engineering > GATE 2020 > Aerodynamics
A Pilot tube mounted on the wing tip of an airplane flying at an altitude of 3 km measures a pressure of 0.72 bar, and the outside air temperature is 268.66 K. Take the sea level conditions as, pressure =1.01 bar, temperature =288.16 K and density =1.225 kg/m³. The acceleration due to gravity is 9.8 m/s² and the gas constant is 287 J/(kg K). Assuming standard atmosphere, the equivalent airspeed for this airplane is _______ m/s (round off to two decimal place).

Correct : 57.10 to 60.00

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airplane wing pressure measurement GATE Aerospace Engineering 2020 pilot tube pressure measurement standard atmosphere calculation equivalent airspeed calculation aerospace engineering gate pressure altitude conversion airspeed standard atmosphere GATE 2020 question 27

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