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Source Panel Method: Normal Velocity Geometric Integral [I(ij)]
Lecture 14 - Source Panel Method (3/01/2021)
Source Panel Method: Circular Cylinder
Vortex Panel Method: Airfoil
Source Panel Method: Tangential Velocity Geometric Integral [J(ij)]
Airfoil Analysis . Vortex Panel Method . Development
14 UofSC Spring 2021 EMCH 578 (03/01/21) Source Panel Method