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Karman Vortex street behind an airfoil (NACA 4412)
NACA4412 Airfoil flow visualization
NACA 4412 Reattached Flow
ME EN 6700 - Flow Visualization on NACA 0012
Wind Tunnel Simulation with NACA 4412 Airfoil
DNS Re=400000 NACA4412
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Last Updated: October 1, 2026
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Summary
At RPI low speed JEC wind tunnel. Angle of attack 20 degrees. Vortex shedding smoke and laser Here's an example of the a CFD of a non-symmetric airfoil such as the Submission to APS DFD Gallery of Fluid Motion 2015. A three dimensional direct numerical simulation using high-order methods ...