NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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
Document Type
Other
Authors
Pinkel, I Irving
Date Acquired
September 6, 2013
Publication Date
January 1, 1948
Report/Patent Number
NACA-TR-907
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19930091974.pdf STI