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Computer simulation of high-frequency combustion instability and its supressionProgram for simulation of gas motion illustrates the effects of some of the variables on the combustion chambers of liquid propellant rocket engines. The program is based on numerically integrating the laws of inviscid fluid dynamics by two-step Lax-Wendroff technique.
Document ID
19690000364
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bucher, R. E.
Date Acquired
August 5, 2013
Publication Date
September 1, 1969
Subject Category
Mathematics And Information Sciences
Report/Patent Number
HQN-10391
Report Number: HQN-10391
Accession Number
69B10368
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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