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Airflow distribution control for improved turbine engine performanceControl allows significant diffuser length and weight reduction, reduces combustor exhaust emissions during engine idle, and improves combustor altitude relight capability.
Document ID
19720000178
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Juhasz, A. J.
Holdeman, J. D.
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Subject Category
Machinery
Report/Patent Number
LEW-11593
Report Number: LEW-11593
Accession Number
72B10178
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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