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The ghost fluid method allows a propagating interface to remain sharp during a numerical simulation. The solution of the Riemann problem at the interface provides proper information to determine interfacial fluxes as well as the velocity of the phase boundary. Then considering …

In this paper we present experimental and numerical reference data for a NACA 64A-110 airfoil at two angles of attack for M a = 0.72 and a Reynolds number of Rec = 930 000 with respect to the chord length. The test cases are designed to provide data for an uninclined airfoil at …