1.

The flight mach number is inversely proportional to relative pressure.(a) True(b) FalseThe question was asked by my college professor while I was bunking the class.The above asked question is from Climb Rate in section Climb and Descent Performance of Aircraft Performance

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Right ANSWER is (a) True

The explanation is: The flight MACH number is inversely proportional to relative pressure. This STATES that the flight mach number increases with DECREASE in relative pressure and decreases WIT increase in relative pressure.



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