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Pilot escape from spinning airplanes as determined from free-spinning-tunnel tests
- Author / Creator
- Available as
- Online
- Summary
-
Procedure for pilot escape from spinning airplanes has been determined by means of tests in which pilot escape was simulated from 21 airplane models spinning in the Langley 20-foot free-spinning tu...
Procedure for pilot escape from spinning airplanes has been determined by means of tests in which pilot escape was simulated from 21 airplane models spinning in the Langley 20-foot free-spinning tunnel. The results in general indicated that the pilot should bail out of the outboard side. Calculated centripetal accelerations acting on the pilot during a spin are presented.
Details
- Creator
- by Stanley H. Scher
- Format
- Books
- Language
- English
- Contributors
- Publication
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- Washington, D.C. : National Advisory Committee for Aeronautics, 1951
- Physical Details
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- 1 online resource (36 pages) : illustrations, tables
- data file
- OCLC
- on1336511439
- "Langley Aeronautical Laboratory."
- Title from title screen (viewed July 14, 2022)
- Date of issue: October 1951.
- Report numbers NACA-TN-2485.
- Includes bibliographical references (page 14)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.