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  • AIRCRAFT  (4)
  • 1970-1974  (4)
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  • 1
    Publication Date: 2019-06-27
    Description: A summary was made of all NASA (and NACA) research and experience related to the spin and recovery characteristics of light personal-owner-type general-aviation airplanes. Very little of the research deals with light general-aviation airplanes as such, but many of the airplanes and models tested before and during World War II were similar to present-day light general-aviation airplanes with regard to the factors that are important in spinning. The material is based mainly on the results of spin-tunnel tests of free-spinning dynamically scaled models of about 100 different airplane designs and, whenever possible, includes correlation with full-scale spin tests. The research results are discussed in terms of airplane design considerations and the proper use of controls for recovery.
    Keywords: AIRCRAFT
    Type: NASA-TN-D-6575 , L-7952
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: Wind tunnel tests, analytical methods and fixed base simulation for predicting fighter aircraft spin characteristics
    Keywords: AIRCRAFT
    Type: AIAA PAPER 70-565 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ATMOSPHERIC FLIGHT MECHANICS CONFERENCE; May 13, 1970 - May 15, 1970; TULLAHOMA, TN
    Format: text
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  • 3
    Publication Date: 2019-07-13
    Description: The present paper discusses the NASA Langley Research Center stall/spin research program to improve the design and the evaluation techniques relative to stall/spin characteristics of general-aviation aircraft. The program encompasses model wind-tunnel tests, spin-tunnel and radio-control model tests, and full-scale airplane spin tests. Initial spin-tunnel results on models with several tail designs representative of light airplanes and several testing techniques are discussed.
    Keywords: AIRCRAFT
    Type: SAE PAPER 730320 , Business Aircraft Meeting; Apr 03, 1973 - Apr 06, 1973; Wichita, KS
    Format: text
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  • 4
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Description of a program aimed at improving the design and evaluation techniques relative to stall/spin characteristics of general-aviation aircraft. The program encompasses analytical studies, full-scale and model wind-tunnel tests, a radio-control model, and full-scale flight tests. Initial spin-tunnel results of several tail designs on a representative light aircraft are discussed.
    Keywords: AIRCRAFT
    Type: SAE PAPER 740354 , Business Aircraft Meeting; Apr 02, 1974 - Apr 05, 1974; Wichita, KS
    Format: text
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