NASA NTRS · 19730021933
Swirl can primary combustor
Abstract
A swirl can full annulus combustor, operable over a wide range of exit average temperatures is used in a high performance gas turbine engine for advanced aircraft. A large number of swirl can modules are mounted in an array in each combustor.
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Jones, R. E., Niedzwiecki, R. W.. 1973-07-31. Swirl can primary combustor. https://ntrs.nasa.gov/citations/19730021933
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