A MUSCL and WENO - PNS Approach for Vortex Dominated Flowfields
Author:
Affiliation:
1. University of Sheffield
2. Sheffield University Aerodynamics and Thermofluids Group
3. Defence Schience & Technology Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-503
Reference33 articles.
1. 1Qin N., Zhong B., Ludlow D.K., Shaw S.T., Birch T.J. "Multigrid acceleration of a matrix-free preconditioned GMRES implicit PNS solver",37thAerospaceScienceMeeting,Reno,Nevada,AIAA99-0779,1999
2. 3Birch T.J., Prince S., Ludlow D.K. and Qin N. "The application of a parabolized Navier-Stokes solver to some hypersonic flowproblems", AIAA2001-1753.
3. Numerical/experimental study of a wingtip vortex in the near field
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