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Recent content by slurped
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Really lost! Vortex Panel Method
Hey! I'm asked to compute the pressure coefficient distributions ܿfor the upper and lower surfaces of a NACA0012 airfoil based on the experimental data provided, which is the one I'm attaching in the image. Then, I have to calculate the lift coefficient distributions ܿand the airfoil global lift...- slurped
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- Replies: 0
- Forum: Computational Fluid Dynamics (CFD)
