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One-dimensional two-phase reacting gas nonequilibrium performance program Interim analysis reportComputer program for calculating inviscid one-dimensional equilibrium, frozen and nonequilibrium nozzle expansion of propellant exhaust mixtures
Document ID
19660021243
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cherry, S. S.
Kliggel, J. R.
Date Acquired
August 3, 2013
Publication Date
May 10, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
TRW-5435-6009-RO-000
NASA-CR-65417
Report Number: TRW-5435-6009-RO-000
Report Number: NASA-CR-65417
Accession Number
66N30533
Funding Number(s)
CONTRACT_GRANT: NAS9-4358
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOZZLE EXPANSION
COMPUTER PROGRAM
INVISCID FLOW
ONE-DIMENSIONAL FLOW

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