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Sub-Sonic Flow over a NACA 5012 Airfoil
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1
Statistics
0 Geometries
1 Mesh
1 Simulation setup
5 Results
0 Geometries 1 Mesh 1 Simulation setup 5 ResultsAbout this project
Simulate the airfoil under the following conditions: The initial pressure is 0 Pa gauge Fluid properties are constant The flow is incompressible and laminar
