General Formulas and Charts for the Calculation of Airplane Performance
Description:
This report presents general formulas for the determination of all major airplane performance characteristics. A rigorous analysis is used, making no assumption regarding the attitude of the airplane at which maximum rate of climb occurs, but finding the attitude at which the excess thrust horsepower is maximum. Equations and charts are developed which show the variation of performance due to a change in any of the customary design parameters.
Date:
1932
Creator:
Oswald, W. Bailey
Item Type:
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Partner:
UNT Libraries Government Documents Department