IMECH-IR  > 力学所知识产出(1956-2008)
高超声速乘波飞行器气动实验研究
Alternative TitleAn 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
Volume23Issue:6Pages:82-85,90
ISSN1000-1328
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 ByCSCD
Language中文
CSCD IDCSCD:1122363
Citation statistics
Document Type期刊论文
Identifierhttp://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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