Question
An aircraft is flying at Mach 0.8 at 5000 [m] altitude. The following information is given. Ratio of specific heats of air: 1.4 Specific
An aircraft is flying at Mach 0.8 at 5000 [m] altitude. The following information is given. Ratio of specific heats of air: 1.4 Specific gas constant of air: 287.05 [m/s KJR Air density at 5000 [m]: 0.7361 [kg/m] Temperature at 5000 [m]: 255.65 [K]T Calculate the energy height of this aircraft?
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Fundamentals Of Aerodynamics
Authors: John Anderson
6th Edition
1259129918, 978-1259129919
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