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Preliminary analysis of selected gas dynamic problemsThe VAST computer code was used to analyze SSME main combustion chamber start-up transients and the IUS flow field for a damaged nozzle was investigated to better understand the gas dynamic considerations involved in vehicle problems, the effect of start transients on the nozzle flow field for the SSME, and the possibility that a damaged nozzle could account for the acceleration anomaly noted on IUS burn. The results obtained were compared with a method of characteristics prediction. Pressure solutions from both codes were in very good agreement and the Mach number solution on the nozzle centerline deviates substantially for the high expansions for the SSME. Since this deviation was unexpected, the phenomenon is being further examined.
Document ID
19850011051
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Prozan, R. J.
(Continuum, Inc. Huntsville, AL, United States)
Farmer, R. C.
(Continuum, Inc. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
January 21, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-171343
CI-FR-0081
NAS 1.26:171343
Report Number: NASA-CR-171343
Report Number: CI-FR-0081
Report Number: NAS 1.26:171343
Accession Number
85N19361
Funding Number(s)
CONTRACT_GRANT: NAS8-35328
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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