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An analytical study of the longitudinal response of airplanes to positive wind shearThe longitudinal response of jet transport aircraft to vertical variation of the horizontal winds is analyzed. Specific reference is given to the role of the speed (u) stability derivatives in the interaction of the airplane and its environment. The relative importance of the u stability derivatives is determined. The wind shear tolerance factor is found which can be used to determine, in a qualitative manner, the stability (tolerance) of an airplane to wind shear. A further study of the control problem shows that the criteria for good control could be reduced from two to one automatic control systems. Only a speed control system is necessary for good control in wind shear.
Document ID
19810011554
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sherman, W. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Aircraft Stability And Control
Report/Patent Number
L-13623
NASA-TP-1765
Report Number: L-13623
Report Number: NASA-TP-1765
Accession Number
81N20082
Funding Number(s)
PROJECT: RTOP 505-44-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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