Item Details

Exploratory Wind-Tunnel Investigation of Deployable Flexible Ventral Fins for Use as an Emergency Spin-Recovery Device

by Sanger M. Burk, Jr.
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, 1971.
Language
English
Series
NASA Tn
Abstract
Spin-tunnel tests have been conducted on dynamic models of two fighter airplanes to explore the feasibility of using deployable flexible ventral fins as an emergency spin-recovery device. Various fin configurations, deflections, and locations were tested. The results indicated that the fins provided satisfactory spin recoveries for the models tested.
Description
33 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared by Langley Research Center.
  • N 71-37603.
Series Statement
NASA TN ; D-6509
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Exploratory wind-tunnel investigation of deployable flexible ventral fins for use as an emergency spin-recovery device / c| by Sanger M. Burk, Jr.
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    a| 33 p. : b| ill. ; c| 28 cm.
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    a| Prepared by Langley Research Center.
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    a| Spin-tunnel tests have been conducted on dynamic models of two fighter airplanes to explore the feasibility of using deployable flexible ventral fins as an emergency spin-recovery device. Various fin configurations, deflections, and locations were tested. The results indicated that the fins provided satisfactory spin recoveries for the models tested.
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Aeronautics x| Safety measures.
    650
      
    0
    a| Airplanes x| Control surfaces.
    650
      
    0
    a| Wind tunnels.
    650
      
    0
    a| Spin (Aerodynamics)
    710
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    a| Langley Research Center.
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    a| United States. b| National Aeronautics and Space Administration.
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    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106954073 y| 1971 r| pd q| bib

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