Item Details

Experimental Study of Acoustic Loads on Upper-Surface-Blown STOL Airplane Configuration

Conrad M. Willis and James A. Schoenster
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1577
Description
54 p. : ill. ; 27 cm.
Notes
  • "December 1979"--Cover.
  • "Langley Research Center."
  • Includes bibliographical references.
Series Statement
NASA technical paper 1577
Technical Details
  • Access in Virgo Classic

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    a| Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration / c| Conrad M. Willis and James A. Schoenster.
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    a| Airplanes x| Testing.
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    a| Jet flaps (Airplanes) x| Testing.
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    a| Airplanes x| Fuselage x| Testing.
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    a| Acoustical engineering.
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