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高超声速乘波飞行器气动实验研究 | |
Alternative Title | An aerodynamic experiment research of the hypersonic waverider vehicle |
姚文秀; 雷麦芳; 杨耀栋; 王发民 | |
Source Publication | 宇航学报 |
2002-12-10 | |
Volume | 23Issue:6Pages:82-85,90 |
ISSN | 1000-1328 |
Abstract | 以绕楔高超声速流场为基础,用流线追踪法生成了一种高超声速飞行器气动概念构形、初步探索了高超声速飞行器机身/推进系统一体化气动构形设计方法,开展了高超声速测压实验,结果表明:该类构形飞行器在高超声速飞行时,可以产生较高的升阻比,前体的预压缩效果明显,是以吸气式冲压发动机动力的有效途的飞行器构形。 |
Keyword | 乘波飞行器 气动构形 气动实验 预压缩性能 |
Indexed By | CSCD |
Language | 中文 |
CSCD ID | CSCD:1122363 |
Citation statistics |
Cited Times:9[CSCD]
[CSCD Record]
|
Document Type | 期刊论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/42314 |
Collection | 力学所知识产出(1956-2008) |
Corresponding Author | 姚文秀 |
Recommended Citation GB/T 7714 | 姚文秀,雷麦芳,杨耀栋,等. 高超声速乘波飞行器气动实验研究[J]. 宇航学报,2002,23,6,:82-85,90. |
APA | 姚文秀,雷麦芳,杨耀栋,&王发民.(2002).高超声速乘波飞行器气动实验研究.宇航学报,23(6),82-85,90. |
MLA | 姚文秀,et al."高超声速乘波飞行器气动实验研究".宇航学报 23.6(2002):82-85,90. |
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