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SoftwareExcercise2

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jurczakmegan
jurczakmegan
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geometries 0 Geometriesmeshes 1 Meshsimulations 1 Simulation setupruns 5 Results
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n this exercise, we will examine the subsonic flow over a NACA 5012 airfoil at two different Reynoldsnumbers

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Project History

  • jurczakmegan

    jurczakmegan created this project