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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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1329 |
| Subjects: | |
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| Call Number: |
NACA TN 1329 |
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