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- W3173467496 abstract "An implicit finite-difference scheme is presented for the efficient computation of unsteady potential flow about airfoils. The formulation uses density and the velocity potential as dependent variables and is cast in conservation form to assure the theoretically correct determination of shockwave location and speed. To enable boundary conditions to be imposed directly on the airfoil surface, a time-varying sheared-rectilinear coordinate transformation is employed. Calculated time-history solutions on a pulsating airfoil are compared with the results of other unsteady transonic codes, including a previous method of the authors. The present method is demonstrated to be unconditionally stable and to give accurate solutions with sharply resolved shocks." @default.
- W3173467496 created "2021-07-05" @default.
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- W3173467496 date "1981-01-12" @default.
- W3173467496 modified "2023-09-26" @default.
- W3173467496 title "An alternating-direction implicit algorithm for unsteady potential flow" @default.
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- W3173467496 doi "https://doi.org/10.2514/6.1981-329" @default.
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