Abstract
A method of calculating transonic separated flows past arbitrary inlets at incidence and yaw is presented. The inviscid flow solver is based on the transonic potential equation, which is approximated and solved numerically on a boundary-conforming coordinate system. The multrigrid finite-volume method is used to solve the flow equation. The inviscid flow technique is coupled with an interactive boundary-layer method that uses an inverse formulation to calculate shock-induced separated flows
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