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An analysis of the limit-cycle and structural- resonance characteristics of the X-15 stability augmentation systemLimit cycle and control surface resonance characteristics of X-15 stability augmentation system
Document ID
19680002077
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Smith, J. W. (NASA Flight Research Center Edwards, CA, United States)
Taylor, L. W., Jr. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4287
Report Number: NASA-TN-D-4287
Accession Number
68N11545
Funding Number(s)
CONTRACT_GRANT: 719-04-05-00-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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