Abstract
AbstractInviscid transonic flow over a wavy wall with either subsonic or supersonic freestream speeds is studied by solving the Euler equations numerically. The streamwise flow development through a series of shock waves and entropy production are investigated in depth. In the case of supersonic freestream, isentropy contours of both horseshoe and staircase forms are found. The limitations and validity of this inviscid rotational flow model are discussed by comparing the results with those for viscous turbulent flow calculated previously.
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