IMECH-IR  > 力学所知识产出(1956-2008)
高超声速流动中侧向喷流干扰特性的实验研究
Alternative TitleExperimental investigations of lateral jet interaction in hypersonic flows
赵桂林; 彭辉; 胡亮; 张绵纯
Source Publication空气动力学学报
2005-06-28
Volume23Issue:2Pages:188-194
ISSN0258-1825
Abstract在高超声速(M=6)流动中,实验研究了侧向喷流的干扰特性,并探讨了喷流压力、攻角、迎风侧及背风侧喷流对侧向喷流干扰特性的影响.结果表明,在高超声速流动中,随喷流压力增大,喷流弓形激波与来流弓形激波相交,喷流前的高压区增大,而喷流后的低压区几乎不受影响,喷流的控制效果加强.与迎风侧喷流相比,背风侧喷流控制效果更好,这一趋势随攻角的增大更加明显.
Keyword侧向喷流 喷流控制 干扰特性 高超声速流动
Indexed ByCSCD
Language中文
CSCD IDCSCD:1993738
Citation statistics
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/41754
Collection力学所知识产出(1956-2008)
Corresponding Author赵桂林
Recommended Citation
GB/T 7714
赵桂林,彭辉,胡亮,等. 高超声速流动中侧向喷流干扰特性的实验研究[J]. 空气动力学学报,2005,23(2):188-194.
APA 赵桂林,彭辉,胡亮,&张绵纯.(2005).高超声速流动中侧向喷流干扰特性的实验研究.空气动力学学报,23(2),188-194.
MLA 赵桂林,et al."高超声速流动中侧向喷流干扰特性的实验研究".空气动力学学报 23.2(2005):188-194.
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