NASA NTRS · 19720000178
Airflow distribution control for improved turbine engine performance
Abstract
Control allows significant diffuser length and weight reduction, reduces combustor exhaust emissions during engine idle, and improves combustor altitude relight capability.
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Juhasz, A. J., Holdeman, J. D.. 1972-05-01. Airflow distribution control for improved turbine engine performance. https://ntrs.nasa.gov/citations/19720000178
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