Numerical solutions of Direct Simulation Monte Carlo (DSMC) method are obtained for axisymmetric supersonic free jet in the transition region (K(sub n infinity) approximately to 0.1). The effects of parameters such as the number density of simulation particles and cell division upon the solution are examined, and pitot pressure calculated from the numerical solution is compared with the experimental data obtained by Askenas and Sherman.
DSMC法による超音速自由噴流の数値計算
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