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Integral Boundary Layer Model for Airfoils by rahpooye313 is a document available to read on EtoBox.

What is Integral Boundary Layer Model for Airfoils about?

1. The document describes an integral boundary layer model that has been added to a panel method code to compute the drag of airfoils in incompressible viscous flow. The boundary layer model is one-way coupled and does not account for the effect of the boundary layer on the inviscid flow. 2. Special characteristics of the one-way coupled model include an unrealistic high adverse pressure gradient at the trailing edge, which can cause early boundary layer separation. To address this, the boundary layer is n

Author

rahpooye313

Language

EN