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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.
Connect to full text Available online
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- Book
- Government document
- Author/Creator:
- Scher, Stanley H., author.
- Series:
- Technical note (United States. National Advisory Committee for Aeronautics) ; 3611.
- Technical notes / National Advisory Committee for Aeronautics ; No. 3611
- Language:
- English
- Subjects (All):
- Airplanes--Testing.
- Airplanes.
- Spin (Aerodynamics).
- Wind tunnel testing.
- Physical Description:
- 1 online resource (54 pages) : illustrations.
- Place of Publication:
- Washington, [D.C.] : National Advisory Committee for Aeronautics, 1956.
- Summary:
- In order to obtain a broader understanding of the factors which affect spin and recovery motions, a technique has been devised for determining the histories of the attitudes and velocities of free-spinning tunnel models from film taken by two motion-picture cameras operating simultaneously. This paper presents the method devised and the results of an initial application of the method in which time histories of attitudes and velocities have been determined for one medium-attitude, moderately oscllatory, developed spin and the recovery therefrom for a model representative of a contemporary fighter airplane.
- Notes:
- Title from title screen (viewed June 7, 2019).
- "April 1956."
- "Langley Aeronautical Laboratory, Langley Field, Va."
- No Federal Depository Library Program (FDLP) item number.
- Includes bibliographical references (page 22).
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
- Other Format:
- Print version: Scher, Stanley H., 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 /
- OCLC:
- 1104148324
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