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# Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method

@inproceedings{JohnTransonicSO, title={Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method}, author={John and W... and Edwards} }

A viscous-inviscid interactive coupling method is used for the computation of unsteady transonic flows involving separation and reattachment. A lag-entrainment integral boundary layer method is used with the transonic small disturbance potential equation in the CAPTSDV code. Efficient and robust computations of steady and unsteady separated flows, including steady separation bubbles and self-excited shock-induced oscillations are presented. The buffet onset boundary for the NACA 0012 airfoil is… CONTINUE READING

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