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Analysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel / by Stanley H. Scher.

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Record details

  • Physical Description: 1 online resource (54 pages) : illustrations.
  • Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1956.

Content descriptions

General Note:
"April 1956."
No Federal Depository Library Program (FDLP) item number.
Bibliography, etc. Note:
Includes bibliographical references (page 22).
Source of Description Note:
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 12, 2020).
Subject: Airplanes > Testing.
Spin (Aerodynamics)
Wind tunnel testing.

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