NASA NTRS · 19850011051
Preliminary analysis of selected gas dynamic problems
Abstract
The 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.
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Prozan, R. J., Farmer, R. C.. 1985-01-21. Preliminary analysis of selected gas dynamic problems. https://ntrs.nasa.gov/citations/19850011051
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