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V2. A plane cruising at an altitude of 5000 m (air temperature -17.5 C pressure 54.0299 kPa density 0.7361 kg/m3 ). If the dash speed dial shows 220 knot determine the hydrodynamic pressure reading of the Pitot tube in kPa including five significant figures. An air knot is 1.852 km/hr.

V2. A plane cruising at an altitude of 5000 m (air temperature -17.5 C pressure 54.0299 kPa density 0.7361 kg/m3 ). If the dash speed dial shows 220 knot determine the hydrodynamic pressure reading of the Pitot tube in kPa including five significant figures. An air knot is 1.852 km/hr.

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V2. A plane cruising at an altitude of 5000 m (air temperature -17.5 C pressure 54.0299 kPa density 0.7361 kg/m3 ). If the dash speed dial shows 220 knot determine the hydrodynamic pressure reading of the Pitot tube in kPa including five significant figures. An air knot is 1.852 km/hr. Answer:
Transcribed Image Text:V2. A plane cruising at an altitude of 5000 m (air temperature -17.5 C pressure 54.0299 kPa density 0.7361 kg/m3 ). If the dash speed dial shows 220 knot determine the hydrodynamic pressure reading of the Pitot tube in kPa including five significant figures. An air knot is 1.852 km/hr. Answer:
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