Study based on fundamental equations of flight and propeller data contained in reports of Nat. Advisory Committee for Aeronautics. It is concluded that under best conditions and assuming that data available could be proportionally reproduced at high altitudes, aeroplane could be designed to give speed of 260 m.p.h. at about 50, 000 ft. altitude.
Factors involved in high airplane speed at great altitudes
Jl. Soc. Automotive Engrs
Society of Automotive Engineers -- Journal ; 6 , n 4 ; p 203-207
1920
5 pages
7 Figs.
Aufsatz (Zeitschrift)
Englisch
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Maintaining airplane engine power at great altitudes
Engineering Index Backfile | 1920
|MAINTAINING AIRPLANE ENGINE POWER AT GREAT ALTITUDES
SAE | 1920
|Operation of airplane motors at high altitudes
Engineering Index Backfile | 1919
|