An aircraft is flying at Mach 0.8 at 5000 [m] altitude. The following information is given....

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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? 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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Calculating the Energy Height of the Aircraft The energy height H of an aircraft represents the tota... View the full answer