超音速流动中侧向喷流干扰特性的实验研究

IMECH-IR > 力学所知识产出(1956-2008)

	超音速流动中侧向喷流干扰特性的实验研究
Alternative Title	EXPERIMENTAL INVESTIGATIONS OF LATERAL JET INTERACTIONS IN SUPERSONIC FLOWS
	赵桂林; 彭辉; 胡亮; 张绵纯
Source Publication	力学学报
	2004-09-19
Volume	36 Issue:5 Pages:577-582
Abstract	在超音速流动中,进行了侧向喷流干扰特性的实验研究,研究了喷流压力、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,随喷流压力增大,喷流前的高压区向前扩展,喷流的包裹作用加强.有攻角时,背风侧喷流前的高压区更大,喷流包裹作用的影响区域前移,喷流的控制效果更好,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超音速流动实验研究
Indexed By	CSCD
Language	中文
CSCD ID	CSCD:1690018
Citation statistics	Cited Times:6[CSCD] [CSCD Record]
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/42174
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. 超音速流动中侧向喷流干扰特性的实验研究[J]. 力学学报,2004,36,5,:577-582.
APA	赵桂林,彭辉,胡亮,&张绵纯.(2004).超音速流动中侧向喷流干扰特性的实验研究.力学学报,36(5),577-582.
MLA	赵桂林,et al."超音速流动中侧向喷流干扰特性的实验研究".力学学报 36.5(2004):577-582.

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