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WIND-TUNNEL INVESTIGATION OF TAIL BUFFET AT SUBSONIC AND TRANSONIC SPEEDS EMPLOYING A DYNAMIC ELASTIC AIRCRAFT MODELWind tunnel investigation of tail buffet at subsonic and transonic speeds
Document ID
19620005297
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cornette, E. S. (NASA Langley Research Center Hampton, VA, United States)
Rigby, R. N. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1962
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1362
Report Number: NASA-TN-D-1362
Accession Number
62N15297
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL
TRANSONIC SPEED
BUFFETING
TAIL

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