NASA NTRS · 19830035522
Combustion response to compositional fluctuations
Abstract
A mechanism involving compositional fluctuations at certain frequencies is examined by which the heterogeneity of a composite solid propellant may contribute directly to the combustion response function of combustion instability theory. A combustion model appropriate to ammonium perchlorate (AP) is used to derive the combustion response to compositional fluctuations, and the properties of the combustion response are discussed in terms of the theoretical results obtained. The concentration exponent, i.e., the dependence of the burn rate on AP concentration, is found to be a signficant combustion parameter and to have a tremendous range of variability. It is suggested that the combustion response to compositional fluctuations may be a dominating factor in driving combustion instability.
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Cohen, N. S., Strand, L. D.. 1983-01-01. Combustion response to compositional fluctuations. https://ntrs.nasa.gov/citations/19830035522
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