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One-dimensional reacting gas nonequilibrium performance program Interim analysis reportComputer program for calculating inviscid one- dimensional nonequilibrium nozzle expansion of propellant exhaust mixtures containing C, H, O, N, F, and Cl
Document ID
19660011697
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kliegel, J. R.
Date Acquired
August 3, 2013
Publication Date
April 17, 1965
Subject Category
Computers
Report/Patent Number
NASA-CR-65224
TRW-5435-6004-RU-000
Report Number: NASA-CR-65224
Report Number: TRW-5435-6004-RU-000
Accession Number
66N20986
Funding Number(s)
CONTRACT_GRANT: NAS9-4358
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ONE-DIMENSIONAL FLOW
NONEQUILIBRIUM FLOW
COMPUTER PROGRAM
NOZZLE EXPANSION
INVISCID FLOW
ROCKET EXHAUST

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