Process development for grid generations to simulate hypersonic flow around a generic re-entry capsule
After the retirement of the Space shuttle, space agencies around the world have turned to space return capsules for re-entry missions. During re-entry into the atmosphere, the capsule undergoes manoeuvres at extremely high speeds reaching 20 Mach and beyond. At such hypersonic conditions, several...
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| 格式: | Theses and Dissertations |
| 語言: | English |
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2016
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| 在線閱讀: | http://hdl.handle.net/10356/68796 |
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| 機構: | Nanyang Technological University |
| 語言: | English |