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Vortex methods for separated flowsThe numerical solution of the Euler or Navier-Stokes equations by Lagrangian vortex methods is discussed. The mathematical background is presented in an elementary fashion and includes the relationship with traditional point-vortex studies, the convergence to smooth solutions of the Euler equations, and the essential differences between two- and three-dimensional cases. The difficulties in extending the method to viscous or compressible flows are explained. The overlap with the excellent review articles available is kept to a minimum and more emphasis is placed on the area of expertise, namely two-dimensional flows around bluff bodies. When solid walls are present, complete mathematical models are not available and a more heuristic attitude must be adopted. The imposition of inviscid and viscous boundary conditions without conformal mappings or image vortices and the creation of vorticity along solid walls are examined in detail. Methods for boundary-layer treatment and the question of the Kutta condition are discussed. Practical aspects and tips helpful in creating a method that really works are explained. The topics include the robustness of the method and the assessment of accuracy, vortex-core profiles, timemarching schemes, numerical dissipation, and efficient programming. Calculations of flows past streamlined or bluff bodies are used as examples when appropriate.
Document ID
19880016958
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Spalart, Philippe R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:100068
NASA-TM-100068
A-88097
Report Number: NAS 1.15:100068
Report Number: NASA-TM-100068
Report Number: A-88097
Accession Number
88N26342
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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