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Transonic Flow Computations Using Nonlinear Potential MethodsThis presentation describes the state of transonic flow simulation using nonlinear potential methods for external aerodynamic applications. The presentation begins with a review of the various potential equation forms (with emphasis on the full potential equation) and includes a discussion of pertinent mathematical characteristics and all derivation assumptions. Impact of the derivation assumptions on simulation accuracy, especially with respect to shock wave capture, is discussed. Key characteristics of all numerical algorithm types used for solving nonlinear potential equations, including steady, unsteady, space marching, and design methods, are described. Both spatial discretization and iteration scheme characteristics are examined. Numerical results for various aerodynamic applications are included throughout the presentation to highlight key discussion points. The presentation ends with concluding remarks and recommendations for future work. Overall. nonlinear potential solvers are efficient, highly developed and routinely used in the aerodynamic design environment for cruise conditions. Published by Elsevier Science Ltd. All rights reserved.
Document ID
20020078395
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Holst, Terry L.
(NASA Ames Research Center Moffett Field, CA United States)
Kwak, Dochan
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Publication Information
Publication: Progress in Aerospace Sciences
Publisher: Elsevier Science Ltd.
Volume: 36
ISSN: 0376-0421
Subject Category
Fluid Mechanics And Thermodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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