Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Mach numbers form 0.60 to 1.30
By: George T. Carson and Edwin E. Lee
Contributors: Lee, Edwin E; Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 1953
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 86
Subjects: Supersonic nozzles; Ultrasonic testing
Notes: "Langley Research Center."

"December 1981"--Cover

Includes bibiliographical references