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乘波构形和乘波飞行器研究综述 | |
Alternative Title | An overview of the research on waveriders and waverider-derived hypersonic Vehicles |
赵桂林![]() ![]() | |
Source Publication | 力学进展
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2003 | |
Volume | 33Issue:3Pages:357-374 |
ISSN | 1000-0992 |
Abstract | 乘波构形的特点是高升阻比,下表面上的流动是均匀的,因此是推进系统/机身一体化设计的理想候选构形.乘波飞行器是源于乘波构形的高超音速飞行器,利用了乘波构形的高升阻比,并可为吸气发动机提供已知的均匀流场.本文比较全面地总结了乘波构形的生成方法和乘波飞行器的设计方法,介绍了乘波构形的优化方法及影响因素,给出了优化的乘波构形,并介绍了乘波飞行器的研究进展,提出了今后的研究重点. |
Keyword | 乘波构形乘波飞行器 高超音速 |
Subject Area | 力学 |
Indexed By | CSCD |
Language | 中文 |
CSCD ID | CSCD:1317924 |
Citation statistics |
Cited Times:16[CSCD]
[CSCD Record]
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Document Type | 期刊论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/16127 |
Collection | 力学所知识产出(1956-2008) |
Recommended Citation GB/T 7714 | 赵桂林,胡亮,闻洁,等. 乘波构形和乘波飞行器研究综述[J]. 力学进展,2003,33,3,:357-374. |
APA | 赵桂林,胡亮,闻洁,彭辉,&张绵纯.(2003).乘波构形和乘波飞行器研究综述.力学进展,33(3),357-374. |
MLA | 赵桂林,et al."乘波构形和乘波飞行器研究综述".力学进展 33.3(2003):357-374. |
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