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NASA NTRS ยท 19750022104

Experimental clean combustor program noise measurement addendum, phase 1

Abstract

The test results of combustor noise measurements taken with waveguide probes are presented. Waveguide probes were shown to be a viable measurement technique for determining high sound pressure level broadband noise. A total of six full-scale annular combustors were tested and included the three advanced combustor designs: swirl-can, radial/axial, and double annular.

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BibTeXRIS

Emmerling, J. J.. 1975-07-01. Experimental clean combustor program noise measurement addendum, phase 1. https://ntrs.nasa.gov/citations/19750022104

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