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Pressure Distribution over NACA 0012

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Incompressible 2 - Run 2 - SimulationRun
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3D
Incompressible - Run 1 - SimulationRun
SimulationRun
3D
naca 0012 300 - Geometry
Geometry
3D
naca 0012 300 - Geometry
Geometry
3D
naca 0012 300 - Geometry
Geometry
3D
views 8
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asarmad
asarmad
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geometries 3 Geometries
meshes 2 Meshes
simulations 2 Simulation setups
runs 3 Results
About this project

To study pressure distribution over NACA 0012 Airfoil for various Angles of Attack

cfd

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Project History

  • asarmad

    asarmad created this project