The transitional flow over a complicated sphere-bicone figure was simulated by DSMC method. The isotherm and pressure contour were shown in the near-continuum region and the drag coefficient and the pressure coefficient distribution curves of the surface were also presented at different Knudsen numbers and different Mach numbers. Comparison analysis of the drag coefficient was carried out between simulated results and approximation data estimated by the bridging-function formula.
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陈伟芳,王全利,吴雄.再入体过渡区气动特性预测[J].国防科技大学学报,2004,26(1):5-7. CHEN Weifang, WANG Quanli, WU Xiong. Research on Aerodynamic Characteristics of Re-entryFigure in Transition Domain[J]. Journal of National University of Defense Technology,2004,26(1):5-7.