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Software Exercise 2 - NACA5012 airfoil
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0 Geometries 1 Mesh 1 Simulation setup 7 Results
About this project
n this exercise, we will examine the subsonic flow over a NACA 5012 airfoil at two different Reynolds numbers.
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by Ali_ArafatAli_Arafat
Project History
schmidtjaymes created this project