Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes /
The design requirements for airplane tail surfaces that would provide effective control for satisfactory recovery from fully developed spins of personal-owner-type light airplanes have been determined from an analysis of the characteristics of approximately 60 models previously tested in the Langley...
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Main Author: | Neihouse, A. I |
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Corporate Author: | United States National Advisory Committee for Aeronautics |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947
|
Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1329 |
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