[AE - 02] - Computational Aerodynamics II

0078 Structured Multiblock Flow Simulations over Sounding Rocket Configurations Including the Influence of Fins
0887 Simulation Of The Airplane Wake Using The Vortex Method With Turbulence Modeling
0958 Finite Element Supg Parameters Computed From Element Edge Matrices For Compressible Flows
1477 Validation of CFD codes for aerodynamic analysis of launch vehicles and sounding rockets
1810 Evaluation Of Collection Efficiency Methods For Icing Analisys


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