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Design Data for Graphical Construction of Two-Dimensional Sharp-Edge-Throat Supersonic NozzlesDesign data are presented for the graphical construction of two-dimensional sharp-edge-throat supersonic nozzles of minimum length for test-section Mach numbers from 1.20 to 10.00. The method of characteristics used in the design is briefly reviewed.
Document ID
20030065295
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Shames, Harold (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Seashore, Ferris L. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
December 2, 1948
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-E8J12
Report Number: NACA-RM-E8J12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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