Control Wing Test

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Incompressible - Run 1 - AOA 15 degrees - SimulationRun
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3D
Flow Region - Geometry
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3D
Test_Simulation_Control_v1 - Geometry
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3D
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SayanS
SayanS
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geometries 2 Geometries
meshes 1 Mesh
simulations 1 Simulation setup
runs 1 Result
About this project

cfd simulation of a NACA 0012 airfoil with span 0.1m and chord 0.1m

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Project History

  • SayanS

    SayanS created this project

    over 3 years ago

Control Wing Test by SayanS | SimScale