Last edited by Akinolar
Friday, July 24, 2020 | History

3 edition of Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 found in the catalog.

Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7

Rivera, JoseМЃ A.

Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7

by Rivera, JoseМЃ A.

  • 332 Want to read
  • 33 Currently reading

Published by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Flutter (Aerodynamics),
  • Aeroelasticity.,
  • Airplanes -- Wings, Rectangular.

  • Edition Notes

    StatementJose A. Rivera, Jr.
    SeriesNASA technical memorandum -- 4094.
    ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18032071M


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Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 by Rivera, JoseМЃ A. Download PDF EPUB FB2