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Performance characteristics of a single-engine fighter model fitted with an in-flight thrust reverserwind tunnel performance characteristics of single-engine fighter model fitted with in-flight thrust reverser
Document ID
19710027908
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Maiden, D. L. (NASA Langley Research Center Hampton, VA, United States)
Mercer, C. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
L-7824
NASA-TN-D-6460
Accession Number
71N37384
Funding Number(s)
PROJECT: RTOP 126-63-11-45
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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