Abstract
THE Van Leer method of flux-vector splitting for the Euler equations is extended for use on moving meshes and all properties of the original splittings ate maintained. The solution is advanced in time with an implicit, approximately factored algorithm. A subiterative procedure to minimize factorization and linearization errors so that larger time steps can be used is investigated. Subsequent computations are shown for a transonic wing undergoing forced pitching oscillation.
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