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Nonlinear effects in the two-dimensional adaptive-wall outer-flow problemThe importance of nonlinear effects to the solution of two-dimensional adaptive-wall outer-flow problems is presently evaluated by comparing outer-flow solutions computed on the basis of the transonic small perturbation equations with solutions based on the linear Prandtl-Glauert equation. Both methods are applied to simulated measurements of transonic flow past a two-dimensional airfoil in free air. Nonlinear effects are found to be important in the outer-flow solution only where the outer flow included supersonic flow.
Document ID
19900048716
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schairer, Edward T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
May 1, 1990
Publication Information
Publication: Journal of Aircraft
Volume: 27
ISSN: 0021-8669
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0021-8669
Accession Number
90A35771
Distribution Limits
Public
Copyright
Other

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