Calculate new values for the 20 000lb airplane in Problem 27, but now flying at 20 000
Question:
Calculate new values for the 20 000‐lb airplane in Problem 27, but now flying at 20 000 ft density altitude. Plot the values and draw the curve on the graph paper.
Data from in problem 27
A 20 000‐lb propeller airplane at sea‐level standard day has the following data. Calculate its Pr and plot the curve on the graph paper.
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Related Book For
Flight Theory And Aerodynamics
ISBN: 9781119772415
4th Edition
Authors: Joseph R. Badick; Brian A. Johnson
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