Requirements for tail surfaces that would provide effective control for satisfactory recovery from fully developed spins have been determined from analysis of characteristics of approximately 60 models previously tested in Langley spin tunnels. See also Engineering Index 1946 p 24.
Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes
Nat Advisory Committee Aeronautics -- Tech Note
1947
8 pages
3 Supp Plates
Report
English
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Tail-design requirements for satisfactory spin recovery
TIBKAT | 1946
|Tail-design requirements for satisfactory spin recovery
Engineering Index Backfile | 1946
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