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. Performance determination by use of the formulas and charts is rapid and explicit. The results obtained by this performance method have been found to give agreement with flight tests that is, in general, equal or superior to results obtained by present commonly used methods.
General formulas and charts for the calculation of airplane performance
1933-01-01
Miscellaneous
No indication
English
General formulas and charts for calculation of airplane performance
Engineering Index Backfile | 1932
|SAE Technical Papers | 1922
|Engineering Index Backfile | 1922
|Airplane performance and design charts
Engineering Index Backfile | 1921
|