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Reversed cowl-flap thrust augmentorInlet mouthpiece with variable geometry improves low-speed performance of inlet (or ejector) of jet engines by use of reversed cowl-flap mechanism. Flaps can be adjusted mechanically or system can be operated with pressure taps set so pressure on inlet face is always smaller than pressure on back of inlet.
Document ID
19740000046
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Cheng, D. Y.
Date Acquired
August 7, 2013
Publication Date
May 1, 1974
Subject Category
Mechanics
Report/Patent Number
ARC-10754
Report Number: ARC-10754
Accession Number
74B10046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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