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choking effect with busemann airfoil

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e0625598
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geometries 0 Geometriesmeshes 3 Meshessimulations 3 Simulation setupsruns 10 Results

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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

    e0625598 created this project