Title: Algorithm for Unsteady Potential Flow About Airfoils
Abstract: Implicit finite-difference scheme efficiently computes unsteady potential flow about airfoils. Formulation uses density and velocity potential as dependent variables. Conservation form is retained to assure that shock wave location and speed are computed correctly. Scheme fills need for method to calculate efficiently unsteady potential flow about airfoils and to predict flutter and other unsteady aeroelastic phenomena in transonic flow regimes.
Publication Year: 1982
Publication Date: 1982-12-01
Language: en
Type: article
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