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Analysis of a jet in a subsonic crosswindJet exhaust flow effects on aerodynamic characteristics of V/STOL aircraft during transition flight
Document ID
19700002522
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Date Acquired
September 2, 2013
Publication Date
January 1, 1969
Subject Category
Aircraft
Report/Patent Number
NASA-SP-218
Report Number: NASA-SP-218
Accession Number
70N11826
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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