LOW-DENSITY NOZZLE-FLOW BY THE DIRECT SIMULATION MONTE-CARLO AND CONTINUUM METHODS

被引:36
作者
CHUNG, CH
KIM, SC
STUBBS, RM
DEWITT, KJ
机构
[1] NASA,LEWIS RES CTR GRP,MYMA INC,CLEVELAND,OH 44135
[2] UNIV TOLEDO,DEPT CHEM ENGN,TOLEDO,OH 43606
基金
美国国家航空航天局;
关键词
D O I
10.2514/3.23841
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Two different approaches, the direct simulation Monte Carlo (DSMC) method based on molecular gasdynamics, and a finite-volume approximation of the Navier-Stokes equations, which are based on continuum gasdynamics, are employed in the analysis of a low-density gas flow in a small converging-diverging nozzle. The fluid experiences various kinds of flow regimes including continuum, slip, transition, and free-molecular. Results from the two numerical methods are compared with Rothe's experimental data, in which density and rotational temperature variations along the centerline and at various locations inside a low-density nozzle were measured by the electron-beam fluorescence technique. The continuum approach showed good agreement with the experimental data as far as density is concerned. The results from the DSMC method showed good agreement with the experimental data, both in the density and the rotational temperature. It is also shown that the simulation parameters, such as the gas/surface interaction model, the energy exchange model between rotational and translational modes, and the viscosity-temperature exponent, have substantial effects on the results of the DSMC method.
引用
收藏
页码:64 / 70
页数:7
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