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数值模拟
Alternative TitleNumerical simulation on lateral jet interaction in supersonic flows
闻洁; 赵桂林; 胡亮; 彭辉
Source Publication北京航空航天大学学报
2005-06-30
Volume31Issue:6Pages:690-695
ISSN1001-5965
Abstract通过与实验结果的比较验证Fluent软件可以用于超音速流动中侧向喷流干扰特性数值研究.使用Fluent软件对超音速流动中不同喷流压力和攻角下侧向喷流干扰特性进行的数值研究表明,超音速流动中,随喷流压力和负攻角增大,喷流前的高压区明显增大,喷流的控制效果更好.喷流包裹作用的影响范围在90°弹面内.喷流压力增大,喷流包裹作用加强,影响范围增大.
Keyword喷流干扰 超音速流动 数值模拟
Indexed ByEI ; CSCD
Language中文
CSCD IDCSCD:2108001
Citation statistics
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/42248
Collection力学所知识产出(1956-2008)
Corresponding Author闻洁
Recommended Citation
GB/T 7714
闻洁,赵桂林,胡亮,等. 超音速流动中侧向喷流干扰特性的数值模拟[J]. 北京航空航天大学学报,2005,31(6):690-695.
APA 闻洁,赵桂林,胡亮,&彭辉.(2005).超音速流动中侧向喷流干扰特性的数值模拟.北京航空航天大学学报,31(6),690-695.
MLA 闻洁,et al."超音速流动中侧向喷流干扰特性的数值模拟".北京航空航天大学学报 31.6(2005):690-695.
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