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
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
|Statement||George T. Carson and Edwin E. Lee.|
|Series||NASA technical paper -- 1953.|
|Contributions||Lee, Edwin E., Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.|
|The Physical Object|
|Pagination||86 p. :|
|Number of Pages||86|
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