MONTE-CARLO SIMULATION OF ENTRY IN THE MARTIAN ATMOSPHERE

被引：9
|
作者：
HASH, DB
HASSAN, HA
机构：
[1] Mechanical and Aerospace Engineering, North Carolina State University, Raleigh, NC
来源：
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER | 1993年 / 7卷 / 02期
基金：
美国国家航空航天局;
关键词：
D O I：
10.2514/3.411
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
The Direct Simulation Monte Carlo (DSMC) method of Bird is used to investigate the characteristics of low density hypersonic flowfields for typical aerobrakes during Martian atmospheric entry. The method allows for both thermal and chemical nonequilibrium. Results are presented for a 60-deg spherically blunt cone for various nose radii and altitudes.
引用
收藏
页码：228 / 232
页数：5
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