On Transonic Shocks in Two-Dimensional Variable-Area Ducts for Steady Euler System


This paper concerns transonic shocks in compressible inviscid flow passing a twodimensional variable-area duct for the complete steady Euler system. The flow is supersonic at the entrance of the duct, whose boundaries are slightly curved. The condition of impenetrability is posed on the boundaries. After crossing a nearly flat shock front, which passes… (More)
DOI: 10.1137/050642447


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