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3-D Coupled CFD-DSMC Solution Method With Application to the Mars Sample Return Orbiter

机译：应用于火星样品返回轨道器的三维耦合CFD-DsmC求解方法

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摘要

A method to obtain coupled Computational Fluid Dynamics-Direct Simulation Monte Carlo (CFD-DSMC), 3-D flow field solutions for highly blunt bodies at low incidence is presented and applied to one concept of the Mars Sample Return Orbiter vehicle as a demonstration of the technique. CFD is used to solve the high-density blunt forebody flow defining an inflow boundary condition for a DSMC solution of the afterbody wake flow. By combining the two techniques in flow regions where most applicable, the entire mixed flow field is modeled in an appropriate manner.

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作者
Glass, C. E. ; Gnoffo, P. A.;
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年度 2000
页码 1-24
总页数 24
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Computational fluid dynamics; Monte carlo method; Three dimensional flow; Direct numerical simulation; Mars sample return missions; Aerodynamic configurations; Forebodies; Aeroshells; Flow distribution; Blunt bodies; Boundary conditions; Multiphase flow;

机译：计算流体动力学;蒙特卡罗方法;三维流动;直接数值模拟;火星样品返回任务;气动构型;前体;气溶胶壳;流动分布;钝体;边界条件;多相流;

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专利

1. Optimal rendezvous trajectory between Sample Return Orbiter and Orbiting Sample Container in a Mars Sample Return mission [J] . Acta astronautica . 2020,第Juna期

机译：在火星样本返回任务中样本返回轨道器和轨道样本容器之间的最佳会合轨迹
2. An orbit-based remote sensing geological assessment of the CanMars Mars Sample Return Analogue Deployment (MSRAD) landing site situated in the Henry Mountains Basin, near Hanksville, Utah [J] . Tornabene Livio L., Battler Melissa, Choe Byung-Hun, Planetary and space science . 2019,第SEPa期

机译：位于犹他州汉克斯维尔附近的亨利山脉盆地的CanMars Mars样本返回模拟部署（MSRAD）着陆点的基于轨道的遥感地质评估
3. An orbit-based remote sensing geological assessment of the CanMars Mars Sample Return Analogue Deployment (MSRAD) landing site situated in the Henry Mountains Basin, near Hanksville, Utah [J] . Tornabene Livio L., Battler Melissa, Choe Byung-Hun, Planetary and space science . 2019,第Sepa期

机译：基于轨道的轨道遥感地质评估帆布MARS样本返回模拟部署（MSRAD）着陆位于犹他州汉克维尔附近的Henry Mountains Basin
4. A 3-D Coupled CFD-DSMC Solution Method With Application To The Mars Sample Return Orbiter [C] . Christopher E. Glass, Peter A. Gnoffo International Symposium on Rarefied Gas Dynamics . 2001

机译：一种3-D耦合的CFD-DSMC解决方案方法，其应用于MARS样品返回轨道
5. Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle [D] . Boyd, Daniel A. 2018

机译：火星样本返回地面飞行器的空气热力学分析
6. A Method for Choosing the Best Samples for Mars Sample Return [O] . Peter R. Gordon, Mark A. Sephton -1

机译：一种为火星样本返回选择最佳样本的方法
7. A 3-D Coupled CFD-DSMC Solution Method With Application To The Mars Sample Return Orbiter [O] . Christopher Glass And, Christopher E. Glass, Peter A. Gnoffo 2000

机译：应用于火星样品返回轨道器的三维耦合CFD-DsmC解法
8. A 3-D Coupled CFD-DSMC Solution Method With Application to the Mars Sample Return Orbiter [R] . Glass, Christopher E., Gnoffo, Peter A. 2000

机译：应用于火星样品返回轨道器的三维耦合CFD-DsmC解法

3-D Coupled CFD-DSMC Solution Method With Application to the Mars Sample Return Orbiter

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