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Monday, August 10, 2020 | History

2 edition of Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30 found in the catalog.

Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30

George T. Carson

Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30

by George T. Carson

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  • 13 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

    Subjects:
  • Supersonic nozzles.,
  • Ultrasonic testing.

  • Edition Notes

    StatementGeorge T. Carson and Edwin E. Lee.
    SeriesNASA technical paper -- 1953.
    ContributionsLee, Edwin E., Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
    The Physical Object
    Pagination86 p. :
    Number of Pages86
    ID Numbers
    Open LibraryOL17655392M


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Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30 by George T. Carson Download PDF EPUB FB2