NASA NTRS · 19800009863
Combustion stability with baffles, absorbers and velocity sensitive combustion
Abstract
Analytical and computational techniques were developed to predict the stability behavior of liquid propellant rocket combustors using damping devices such as acoustic liners, slot absorbers, and injector face baffles. Models were developed to determine the frequency and decay rate of combustor oscillations, the spatial and temporal pressure waveforms, and the stability limits in terms of combustion response model parameters.
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Mitchell, C. E.. 1980-02-01. Combustion stability with baffles, absorbers and velocity sensitive combustion. https://ntrs.nasa.gov/citations/19800009863
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