| Optimal speed of hypersonic cruise flight | |
Fan J(樊菁)
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| Source Publication | THEORETICAL & APPLIED MECHANICS LETTERS
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| 2011 | |
| Volume | 1Issue:1Pages:012004 |
| ISSN | 2095-0349 |
| Abstract | A coupling frame of speed gain and maintain was suggested to assess the flight performance of hypersonic cruise vehicles (HCV). The optimal cruise speed was obtained by analyzing the flight performance measured by the ratio of initial boost mass to generalized payload. The performance of HCVs based on rockets and air-breathing ramjets was studied and compared to that of a minimum-energy ballistic trajectory under a certain flight distance. It is concluded that rocket-based HCVs flying at the optimal speed are a very competitive choice at the current stage. |
| URL | 查看原文 |
| Language | 英语 |
| Department | LHD微尺度和非平衡流动 |
| Classification | 二类 |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/48735 |
| Collection | 高温气体动力学国家重点实验室 |
| Recommended Citation GB/T 7714 | Fan J. Optimal speed of hypersonic cruise flight[J]. THEORETICAL & APPLIED MECHANICS LETTERS,2011,1(1):012004. |
| APA | Fan J.(2011).Optimal speed of hypersonic cruise flight.THEORETICAL & APPLIED MECHANICS LETTERS,1(1),012004. |
| MLA | Fan J."Optimal speed of hypersonic cruise flight".THEORETICAL & APPLIED MECHANICS LETTERS 1.1(2011):012004. |
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