NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Digital program analyzes supersonic flow field within bell-shaped rocket nozzlesDigital computer program computes and analyzes supersonic flow field in axisymmetric rocket nozzle for specified gas properties, nozzle geometry, and input or starting line. Method of characteristics is used for solution of set of hyperbolic partial differential equations.
Document ID
19700000578
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Elliott, J. J. (N. AM. ROCKWELL CORP.)
Stromsta, R. R.
Date Acquired
August 5, 2013
Publication Date
November 1, 1970
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-14292
Report Number: MFS-14292
Accession Number
70B10597
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available