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NASA NTRS · 19700000310

Swirl-can combustor segment

Abstract

Combustor produces uniform circumferential and radial combustor exit temperature profiles and high combustion efficiency at high temperature loads. Absence of diluent air entry ports eliminates stress concentration points, low pressure fuel alleviates nozzle fouling, and abundant air at all burning stages reduces smoke.

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BibTeXRIS

Jones, R., Moyer, H., Niedzwiecki, R.. 1970-06-01. Swirl-can combustor segment. https://ntrs.nasa.gov/citations/19700000310

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