NASA NTRS · 19690000364
Computer simulation of high-frequency combustion instability and its supression
Abstract
Program 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.
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Bucher, R. E.. 1969-09-01. Computer simulation of high-frequency combustion instability and its supression. https://ntrs.nasa.gov/citations/19690000364
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