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Flight-determined aerodynamic derivatives of the AD-1 oblique-wing research airplaneThe AD-1 is a variable-sweep oblique-wing research airplane that exhibits unconventional stability and control characteristics. In this report, flight-determined and predicted stability and control derivatives for the AD-1 airplane are compared. The predictions are based on both wind tunnel and computational results. A final best estimate of derivatives is presented.
Document ID
19870001438
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sim, A. G. (NASA Ames Research Center Moffett Field, CA, United States)
Curry, R. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1984
Subject Category
Aircraft Stability And Control
Report/Patent Number
H-1179
NASA-TP-2222
NAS 1.60:2222
Report Number: H-1179
Report Number: NASA-TP-2222
Report Number: NAS 1.60:2222
Accession Number
87N10871
Funding Number(s)
PROJECT: RTOP 505-43-44
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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