General Airplane Performance
Description:
"Equations have been developed for the analysis of the performance of the ideal airplane, leading to an approximate physical interpretation of the performance problem. The basic sea-level airplane parameters have been generalized to altitude parameters and a new parameter has been introduced and physically interpreted. The performance analysis for actual airplanes has been obtained in terms of the equivalent ideal airplane in order that the charts developed for use in practical calculations wil…
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Date:
June 1, 1937
Creator:
Rockfeller, W. C.
Partner:
UNT Libraries Government Documents Department