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choking effect with busemann airfoil
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0 Geometries 3 Meshes 3 Simulation setups 10 Results
About this project
this simulation predict the hysteresis phenomena when a buseman airfoil will accelerate above the specific choking mach number and decelerate to sub sonic speed. the simulations will done with rhoCentralFoam with zero viscosity (Euler-Equations) At first a coarse mesh with around 50k cells is used.
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e0625598 created this project