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Aerothermodynamic Optimization of Re- Entry Heat Shield Shapes for a Crew Exploration Vehicle

机译：乘员探查车再入式挡热板形状的空气热力学优化

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《AIAA Guidance, Navigation, and Control Conference》|2006年|P.1-15|共15页
会议地点 Keystone CO(US)
作者
J. Johnson; R. Starkey; M. Lewis;
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作者单位

University of Maryland College Park MD;

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原文格式 PDF
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1. Aerodynamic Stability of Reentry Heat Shield Shapes for a Crew Exploration Vehicle [J] . Joshua E. Johnson, Ryan P. Starkey, Mark J. Lewis Journal of Spacecraft and Rockets . 2006,第4期

机译：乘员探员飞行器折返式隔热板形状的空气动力学稳定性
2. Aerothermodynamic Testing of the Crew Exploration Vehicle at Mach 6 and Mach 10 [J] . Karen T. Berger Journal of Spacecraft and Rockets . 2009,第4期

机译：乘员6马赫和10马赫的乘员探索车的空气热力学测试
3. Aerothermodynamic Testing of the Crew Exploration Vehicle at Mach 6 and Mach 10 [J] . Karen T. Berger Journal of Spacecraft and Rockets . 2009,第4期

机译：乘员6马赫和10马赫的乘员探索车的空气热力学测试
4. Aerothermodynamic Optimization of Re- Entry Heat Shield Shapes for a Crew Exploration Vehicle [C] . American Institute of Aeronautics and Astronautics Guidance, Navigation, and Control Conference . 2006

机译：用于船员勘探车的再入热屏蔽空气动力学优化
5. Aerothermodynamic optimization of Earth entry blunt body heat shields for Lunar and Mars return. [D] . Johnson, Joshua E. 2009

机译：月球和火星返回的地球入口钝体隔热罩的空气热力学优化。
6. Multi-Response Optimization of WEDM Process Parameters for Machining of Superelastic Nitinol Shape-Memory Alloy Using a Heat-Transfer Search Algorithm [O] . Rakesh Chaudhari, Jay J. Vora, S. S. Mani Prabu, 2019

机译：传热搜索算法加工超弹性镍钛诺形状记忆合金的WEDM工艺参数的多响应优化
7. Aerothermodynamic Testing of the Crew Exploration Vehicle in the LaRC 20-Inch Mach 6 and 31-Inch Mach 10 Tunnels [O] . Berger Karen T. 2009

机译：LaRC 20英寸马赫6和31英寸马赫10隧道中乘员探索车的空气热力学测试
8. Aerothermodynamic Testing of Protuberances and Penetrations on the NASA Crew Exploration Vehicle Heat Shield in the NASA Langley 20-Inch Mach 6 Air Tunnel [R] . Liechty, Derek S. 2008

机译：美国航空航天局兰利20英寸mach 6空中隧道Nasa机组探测车热屏上的突起和穿透的气动热力学测试

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