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Exploratory wind-tunnel investigation of deployable flexible ventral fins for use as an emergency spin-recovery deviceSpin tunnel tests to determine effectiveness of deployable, flexible ventral fins for spin recovery device on fighter aircraft
Document ID
19710028127
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Burk, S. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-6509
L-7877
Report Number: NASA-TN-D-6509
Report Number: L-7877
Accession Number
71N37603
Funding Number(s)
PROJECT: RTOP 136-62-02-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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