Technical study of various systems of braking and of devices for shortening landing runs. Reference is made to investigations by Nat. Advisory Committee for Aeronautics, from which investigations it is concluded that for a given size of propeller, wide blades have a larger brake effect than narrow blades, and that brake effect of higher-pitch propeller is less than that of lower-pitch propeller.
Landing run and get-away for standard airplanes
J1. Soc. Automotive Engrs
1920
6 pages
9 Figs.
Article (Journal)
English
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LANDING RUN AND GET-AWAY FOR STANDARD AIRPLANES
SAE Technical Papers | 1920
|Engineering Index Backfile | 1922
|Engineering Index Backfile | 1930
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1930
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