Abstract
An asymptotic method for one-dimensional nozzle flows with nonequilibrium condensation that reveals the structure of possible condensation zones is presented. The streamtube formulation for expansion flows on walls with nonequilibrium condensation employed with the asymptotic method is discussed for both smooth flows and flows with an embedded, frozen, oblique shock wave. In particular the location of the oblique shock wave is predicted by employing Barschdorff’s shock fitting technique. The extension of the method for shock tubes is also summarized.
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