Development of formulas for determination of major airplane performance characteristics making no assumption regarding altitude of airplane at which maximum rate of climb occurs, but finding altitude at which excess thrust horsepower is maximum; performance in terms of parasite loading, effective span loading and thrust horsepower loading.
General formulas and charts for calculation of airplane performance
Nat Advisory Committee Aeronautics -- Report
1932
50 pages
Report
English
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SAE Technical Papers | 1922
|Engineering Index Backfile | 1922
|Airplane performance and design charts
Engineering Index Backfile | 1921
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