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The significance of nonlinear damping trends determined for current aircraft configurationsRigidly forced oscillatory dynamic stability method for measuring pitch and yaw damping derivatives in wind tunnels at transonic and supersonic speeds
Document ID
19680007986
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wiley, H. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 4, 2013
Publication Date
September 1, 1966
Publication Information
Publication: AGARD STABILITY AND CONTROL, PT. 1 SEP. 1966 (SEE N68-17439 08-02)
Subject Category
Aircraft
Accession Number
68N17455
Distribution Limits
Public
Copyright
Other
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