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Some recent developments in predicting unsteady loadings caused by control surface motionsSolution instabilities are identified within the procedures used to predict unsteady loadings due to motions of swept hingeline control surfaces. A preferred solution process that demonstrates the need of calculating smooth residual downwash distributions is described. Numerical results displaying erratic solution behavior when use is made of various forms of pressure expressions currently employed in control surface analyses are presented. A new expression of the asymptotic pressure function is derived, which exactly satisfies the change in boundary conditions around the boundary of the control surface. Results of applying the new pressure function are presented and indicate that stable converged solutions may be achieved for predicting the unsteady loadings caused by motions of swept hingeline control surfaces.
Document ID
19750034237
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rowe, W. S.
Sebastian, J. D.
Redman, M. C.
(Boeing Commercial Airplane Co. Renton, Wash., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 75-101
Report Number: AIAA PAPER 75-101
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 20, 1975
End Date: January 22, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A18309
Funding Number(s)
CONTRACT_GRANT: NAS1-12020
Distribution Limits
Public
Copyright
Other

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