机构

• 工程热物理研究所 [15]
• 力学研究所 [2]
• 数学与系统科学研究院 [1]
• 武汉物理与数学研究所 [1]
• 近代物理研究所 [1]

采集方式

• OAI收割 [20]

内容类型

• 期刊论文 [19]
• 会议论文 [1]

发表日期

• 2019 [2]
• 2016 [3]
• 2015 [1]
• 2010 [6]
• 2006 [1]
• 2005 [1]
• 更多

学科主题

筛选

浏览/检索结果: 共20条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Stability of supersonic contact discontinuity for two-dimensional steady compressible Euler flows in a finite nozzle 期刊论文  OAI收割 JOURNAL OF DIFFERENTIAL EQUATIONS, 2019, 卷号: 266, 期号: 7, 页码: 4337-4376 作者:  Huang, Feimin;  Kuang, Jie;  Wang, Dehua;  Xiang, Wei   |  收藏  |  浏览/下载：27/0  |  提交时间：2019/03/05 Contact discontinuity  Supersonic flow  Free boundary  Compressible Euler equation  Finitely long nozzle   Stability of supersonic contact discontinuity for two-dimensional steady compressible Euler flows in a finite nozzle 期刊论文  OAI收割 JOURNAL OF DIFFERENTIAL EQUATIONS, 2019, 卷号: 266, 期号: 7, 页码: 4337-4376 作者:  Xiang, Wei;  Wang, Dehua;  Kuang, Jie;  Huang, Feimin   |  收藏  |  浏览/下载：34/0  |  提交时间：2019/06/24 Contact discontinuity  Supersonic flow  Free boundary  Compressible Euler equation  Finitely long nozzle   Annular Supersonic Swirling Flows with Heterogeneous Condensation 期刊论文  OAI收割 2016 作者:  Fukushima, Y., Matsuo, S., Shiomi, N. and Setoguchi, T. 收藏  |  浏览/下载：34/0  |  提交时间：2017/05/27 compressible flow heterogeneous condensation homogeneous condensation supersonic nozzle annular swirling flow simulation model Thermodynamics Engineering   Three-Dimensional Rainbow Schlieren Measurements in Underexpanded Sonic Jets from Axisymmetric Convergent Nozzles 期刊论文  OAI收割 2016 作者:  Takano, H., Kamikihara, D., Ono, D., Nakao, S., Yamamoto, H. and Miyazato, Y. 收藏  |  浏览/下载：49/0  |  提交时间：2017/05/27 Rainbow schlieren Computer tomography Convergent nozzle Sonic jet supersonic jets deflectometry Thermodynamics Engineering   Evaluation and optimal design of supersonic nozzle for laser-assisted oxygen cutting of thick steel sections 期刊论文  OAI收割 INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2016, 卷号: 86, 期号: 2016-05-08, 页码: 1243-1251 作者:  Zhang, C;  Wen, P;  Yuan YM(袁越明);  Fan XJ(范学军) 收藏  |  浏览/下载：19/0  |  提交时间：2016/12/08 Laser cutting  Supersonic nozzle  Numerical simulation  Flow visualization   Effect of Nozzle Inlet Shape on Annular Swirling Flow with Non-Equilibrium Condensation 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2015, 卷号: 24, 期号: 4, 页码: 344-349 作者:  Fukushima, Yusuke;  Matsuo, Shigeru;  Setoguchi, Toshiaki;  Shiomi, Norimasa;  Hashimoto, Tokitada 收藏  |  浏览/下载：35/0  |  提交时间：2015/10/27 compressible flow  non-equilibrium condensation  supersonic annular nozzle  swirl flow  simulation   Unsteady Shock-Flow Characteristics in an Over-Expanded Rocket Nozzle 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 4, 页码: 332,336 Jong Sung Lee1; Huey Dong Kim1*; Toshiaki Setoguchi2; Shigeru Matsuo2 收藏  |  浏览/下载：22/0  |  提交时间：2013/01/06 Free shock separation  Over-expansion flow  Restricted shock separation  Side-loads  Supersonic nozzle   Application of Rainbow Schlieren Deflectometry for Axisymmetric Supersonic Jets (Comparison of Experiments with Numerical Analysis) 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 3, 页码: 218,221 Hideki Yamamoto1; Masayuki Irie1; Yoshiaki Miyazatol; Kazuyasu Matsuol 收藏  |  浏览/下载：16/0  |  提交时间：2013/01/06 Rainbow Schlieren Technique  Numerical Analysis  Axisymmetric Nozzle  Correctly-Expanded Supersonic Jet   A Computational Study of Thrust Vectoring Control Using Dual Throat Nozzle 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 6, 页码: 486,490 Choon Sik Shin1; Heuy Dong Kim1; Toshiaki Setoguchi2; Shigeru Matsuo2 收藏  |  浏览/下载：24/0  |  提交时间：2013/01/06 Compressible Flow  Dual Throat Nozzle  Thrust Vector Control  Shock Wave  Supersonic Flow   Hysteretic Phenomenon of Shock Wave in a Supersonic Nozzle 期刊论文  OAI收割 JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 6, 页码: 526,532 Toshiaki Setoguchi1; Shigeru Matsuo2; M.M. Ashraful Alam3; Junji Nagao3; Heuy Dong Kim4 收藏  |  浏览/下载：22/0  |  提交时间：2013/01/06 compressible flow  hysteresis|internal flow  shock wave  supersonic nozzle