摘要
For an approximate design of aerospike nozzle, some numerical and experimental studies and conclusions are given here. The numerical simulations contain of both the Method of Characteristic and the solving of the Navier-Stokes equations. The experimental system and several kinds of the test aerospike nozzle are showed here. Some tests and calculations curves are presented and explained.
源语言 | 英语 |
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出版状态 | 已出版 - 2001 |
已对外发布 | 是 |
活动 | 37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, 美国 期限: 8 7月 2001 → 11 7月 2001 |
会议
会议 | 37th Joint Propulsion Conference and Exhibit 2001 |
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国家/地区 | 美国 |
市 | Salt Lake City, UT |
时期 | 8/07/01 → 11/07/01 |