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

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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

Book details:

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 LibraryOL16807221M

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