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Tuesday, May 12, 2020 | History

2 edition of Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane found in the catalog.

Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane

James L. Dillon

Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane

by James L. Dillon

  • 234 Want to read
  • 8 Currently reading

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

    Subjects:
  • Hypersonic planes.

  • Edition Notes

    StatementJames L. Dillon and Jimmy L. Pittman.
    SeriesNASA technical paper ; 1044, NASA technical paper -- 1044.
    ContributionsPittman, Jimmy L., United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
    The Physical Object
    Pagination73 p. :
    Number of Pages73
    ID Numbers
    Open LibraryOL18013335M


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Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane by James L. Dillon Download PDF EPUB FB2