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Conditions of generation and methods of damping the inlet vortex of a turbojet engineAn aeromechanical analysis of the generation of an inlet vortex in a turbojet engine is presented. Methods for the prevention of vortex generation and methods of vortex damping are described.
Document ID
19820012308
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Gajewski, T. (NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-76678
NAS 1.15:76678
Report Number: NASA-TM-76678
Report Number: NAS 1.15:76678
Accession Number
82N20182
Funding Number(s)
CONTRACT_GRANT: NASW-3541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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