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aerofoil

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gowtham13123
gowtham13123
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In this project we examined the Effect of Boundary Layers on the NACA 0012 Airfoil. In-compressible fluid flow simulation is selected for the project. Free stream velocity is selected as 10 m/s having A.O.A 10 with the airfoil. - Copy

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Project History

  • HamzaBaig

    HamzaBaig created this project

  • gowtham13123

    gowtham13123 copied this project