Commenced in January 2007
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Large-Eddy Simulation of Hypersonic Configuration Aerodynamics
Abstract:LES with mixed subgrid-scale model has been used to simulate aerodynamic performance of hypersonic configuration. The simulation was conducted to replicate conditions and geometry of a model which has been previously tested. LES Model has been successful in predict pressure coefficient with the max error 1.5% besides afterbody. But in the high Mach number condition, it is poor in predict ability and product 12.5% error. The calculation error are mainly conducted by the distribution swirling. The fact of poor ability in the high Mach number and afterbody region indicated that the mixed subgrid-scale model should be improved in large eddied especially in hypersonic separate region. In the condition of attach and sideslip flight, the calculation results have waves. LES are successful in the prediction the pressure wave in hypersonic flow.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1061430Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1279
 DNS of Hypersonic Turbulent Boundary Layers.AIAA-2004-2337.
 Soshi Kawai and Kozo Fujii.. Large-Eddy Simulation of Compressible Transitional Boundary Layer. AIAA-2006-7941.
 Bamdad Lessani. Large-Eddy Simulationof Turbulent Flows. Vrije Universiteit.2003.
 M.Pino Martin. Subgrid-Scale Models for Compressible Large-Eddy Simulation. Theoretical and Computational Fluid Dynamics.2000:361-376.
 Xiao.Hong Liu.zhenxia. Experiment of Hypersonic Vehicle Configuration. AJCPP-2008. A4-1.2008.