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浏览/检索结果: 共5条，第1-5条 帮助 已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Influences of effusion hole diameter on impingement/effusion cooling performance at turbine blade leading edge 期刊论文 INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 134, 页码: 1101-1118 作者:  Zhou, Junfei;  Wang, Xinjun;  Li, Jun 收藏  |  浏览/下载：13/0  |  提交时间：2019/11/19 Numerical simulation  Impingement/effusion cooling  Internal cooling  Gas turbine blade leading edge   EFFECTS OF IMPINGING HOLE SHAPES ON DOUBLE SWIRL COOLING PERFORMANCE AT GAS TURBINE BLADE LEADING EDGE 会议论文 作者:  Zhou, Junfei;  Wang, Xinjun;  Li, Jun;  Zheng, Daren 收藏  |  浏览/下载：2/0  |  提交时间：2019/11/26 swirl cooling  numerical simulation  internal cooling  gas turbine blade leading edge   Effects of film cooling hole locations on flow and heat transfer characteristics of impingement/effusion cooling at turbine blade leading edge 期刊论文 INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2018, 卷号: 126, 页码: 192-205 作者:  Zhou, Junfei;  Wang, Xinjun;  Li, Jun;  Li, Yandong 收藏  |  浏览/下载：16/0  |  提交时间：2019/11/26 Numerical simulation  Impingement/effusion cooling  Internal cooling  Gas turbine blade leading edge   Surface recrystallisation and oxidation of polycrystalline superalloy castings during isothermal exposure at 1100 degrees C 期刊论文 International Journal of Cast Metals Research, 2012, 卷号: 25, 期号: 4, 页码: 195-200 W. G. Jiang; M. C. Yang; L. H. Lou; Z. Q. Hu 收藏  |  浏览/下载：23/0  |  提交时间：2013/02/05 Superalloy  Investment casting  Modulus  Recrystallisation  Residual  stress  Oxidation  ni-base superalloy  gas-turbine blade  heat-treatment  dynamic  recrystallization  leading-edge  water-vapor  microstructure  behavior  900-degrees-c  evolution   Numerical study on flow and heat transfer of impingement cooling on leading edge of actual turbine blade 期刊论文 Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2011, 卷号: 45, 期号: [db:dc_citation_issue], 页码: 5-9+20 作者:  Liu, Zhao;  Feng, Zhenping;  Song, Liming 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/10 Actual blade leading edge  Flow and heat transfer  Gas turbine blades  Impingement cooling  Impinging jet  Jet nozzle diameters  Overall accuracies  Two-equation turbulence models