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BUFFET TESTS OF AN ATTACK-AIRPLANE MODEL WITH EMPHASIS ON ANALYSIS OF DATA FROM WIND-TUNNEL TESTSBuffeting tests of attack aircraft model at transonic speeds
Document ID
19630002658
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Davis, D. D., Jr. (NASA Langley Research Center Hampton, VA, United States)
Wornom, D. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 21, 1958
Subject Category
Aircraft
Report/Patent Number
NACA-RM-L57H13
Report Number: NACA-RM-L57H13
Accession Number
63N12534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BUFFETING
ATTACK AIRCRAFT
DAMPING
AERODYNAMICS
DELTA WING
TRANSONIC SPEED
WIND TUNNEL

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