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