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Equations for the design of two-dimensional supersonic nozzlesEquations are presented for obtaining the wall coordinates of two-dimensional supersonic nozzles. The equations are based on the application of the method of characteristics to irrotational flow of perfect gases in channels. Curves and tables are included for obtaining the parameters required by the equations for the wall coordinates. A brief discussion of characteristics as applied to nozzle design is given to assist in understanding and using the nozzle-design method of this report. A sample design is shown.
Document ID
19930091974
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pinkel, I Irving
Date Acquired
September 6, 2013
Publication Date
January 1, 1948
Report/Patent Number
NACA-TR-907
Accession Number
93R21264
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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