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Description of a computer program to calculate reacting supersonic internal flow fields with shock waves using viscous characteristics: Program manual and sample calculationsA computer program for calculating internal supersonic flow fields with chemical reactions and shock waves typical of supersonic combustion chambers with either wall or mid-stream injectors is described. The usefulness and limitations of the program are indicated. The program manual and listing are presented along with a sample calculation.
Document ID
19730011584
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cavalleri, R. J. (New York Univ. New York, NY, United States)
Agnone, A. M. (New York Univ. New York, NY, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-112303
Report Number: NASA-CR-112303
Accession Number
73N20311
Funding Number(s)
CONTRACT_GRANT: NGR-33-016-131
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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