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WIND-TUNNEL MEASUREMENTS OF AERODYNAMIC DAMPING DERIVATIVES OF A LAUNCH VEHICLE VIBRATING IN FREE-FREE BENDING MODES AT MACH NUMBERS FROM 0.70 TO 2.87 AND COMPARISONS WITH THEORYWind tunnel tests of aerodynamic damping of a launch vehicle
Document ID
19620006102
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Doggett, R. V., Jr. (NASA Langley Research Center Hampton, VA, United States)
Hanson, P. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1962
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1391
Report Number: NASA-TN-D-1391
Accession Number
62N16102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DAMPING
LAUNCH VEHICLE
AERODYNAMICS
WIND TUNNEL

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