Abstract
A time-dependent numerical scheme, in conjunction with a three-dimensional, body-fitted, coordinate transformation technique, is utilized for the solution of subsonic-transonic-supersonic flows-both gas-only, one-phase, and fully coupled, gas-particle, two-phase-inside three-dimensional canted nozzles of arbitrary configurations. No difficulty is encountered with the time-dependent formulation for the solution of mixed transonic flowfield, which has been a bottleneck in many three-dimensional nozzle flow studies
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