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NASA NTRS ยท 19720030288

Combustion stabilization with acoustic cavities.

Abstract

An experimental and analytical study has been performed to develop the technology necessary for effective use of acoustic cavities to suppress acoustic modes of combustion instability. An unbaffled variation of the LM ascent engine has been made dynamically stable with acoustic cavities only; five different cavity configurations were found sufficient to produce dynamic stability. An analytical model was developed to calculate the damping contributed by the cavity. Further, subscale tests were made to determine the nonlinear acoustic impedance of these cavities.

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BibTeXRIS

Oberg, C. L.. 1971-12-01. Combustion stabilization with acoustic cavities.. https://ntrs.nasa.gov/citations/19720030288

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