SIMULATION OF AIRCRAFT WAKE VORTEX USING PRESSURE-BASED UNIFIED NUMERICAL APPROACH FOR INCOMPRESSIBLE AND COMPRESSIBLE FLOWS
Meeting; 42nd, Aerospace sciences; Aerospace sciences 42 ; 2004 ; Reno, NV
01.01.2004
77 pages
Papers 2004-01 - 2004-681 with gaps
Aufsatz (Konferenz)
Englisch
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A Unified Approach for Adaptive Solutions of Compressible and Incompressible Flows
British Library Conference Proceedings | 1997
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