A Computational Study of Thrust Vectoring Control Using Dual Throat Nozzle
文献类型：期刊论文
| 作者 | Choon Sik Shin1; Heuy Dong Kim1; Toshiaki Setoguchi2; Shigeru Matsuo2 |
| 刊名 | JOURNAL OF THERMAL SCIENCE
 |
| 出版日期 | 2010 |
| 卷号 | 19期号:6页码:486,490 |
| 关键词 | Compressible Flow Dual Throat Nozzle Thrust Vector Control Shock Wave Supersonic Flow |
| 英文摘要 | Dual throat nozzle (DTN) is fast becoming a popular technique for thrust vectoring. The DTN is designed with two throats, an upstream minimum and a downstream minimum at the nozzle exit, with a cavity in between the upstream throat and exit. In the present study, a computational work has been carried out to analyze the perform- ance of a dual throat nozzle at various mass flow rates of secondary flow and nozzle pressure ratios (NPR). Two-dimensional, steady, compressible Navier-Stokes equations were solved using a fully implicit finite volume scheme. The present computational results were validated with available experimental data. Based on the present results, the control effectiveness of thrust-vectoring is discussed in terms of the thrust coefficient and the coeffi- cient of discharge. |
| 公开日期 | 2013-01-06 |
| 源URL | [http://ir.etp.ac.cn/handle/311046/51679]  |
| 专题 | 工程热物理研究所_Journal of Thermal Science |
| 推荐引用方式 GB/T 7714 | Choon Sik Shin1,Heuy Dong Kim1,Toshiaki Setoguchi2,et al. A Computational Study of Thrust Vectoring Control Using Dual Throat Nozzle[J]. JOURNAL OF THERMAL SCIENCE,2010,19(6):486,490. |
| APA | Choon Sik Shin1,Heuy Dong Kim1,Toshiaki Setoguchi2,&Shigeru Matsuo2.(2010).A Computational Study of Thrust Vectoring Control Using Dual Throat Nozzle.JOURNAL OF THERMAL SCIENCE,19(6),486,490. |
| MLA | Choon Sik Shin1,et al."A Computational Study of Thrust Vectoring Control Using Dual Throat Nozzle".JOURNAL OF THERMAL SCIENCE 19.6(2010):486,490. |
入库方式： OAI收割
来源：工程热物理研究所
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