Solver and Turbulence Model Upgrades to OVERFLOW 2 for Unsteady and High-Speed Applications
Author:
Affiliation:
1. University of Alabama in Birmingham
2. Digital Fusion
3. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2824
Reference46 articles.
1. 1Murphy,K.J.,Buning,P.G.,Pamadi,B.N.,Scallion,W.I.,andJones,K.M."OverviewofTransonictoHypersonicStage Separation Tool Development for Multi-Stage-to-OrbitConcepts,"AIAA-2004-2595, Jun.2004.
2. 2Buning,P.G.,Gomez,R.J.,andScallion,W.I."CFDApproachesforSimulationofWing-BodyStageSeparation,"AIAA2004-4838, Aug. 2004.
3. A comparative study of turbulence models for overset grids
4. 5Meakin,R.L."ObjectX-RaysforCuttingHolesinCompositeOversetStructuredGrids,"AIAA-2001-2537,Jun.2001.
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