共 50 条
- [41] Numerical investigation of the rotation on the film cooling over a flat surface [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2005, VOL 3 PTS A AND B, 2005, : 527 - 536
- [42] Effect of Prandtl number on leading edge accretion and ablation: A numerical study of unsteady boundary layer flow over a flat plate [J]. HEAT TRANSFER-ASIAN RESEARCH, 2019, 48 (07): : 2844 - 2881
- [43] Numerical simulations of flat plate film cooling using respectively different shaped jet holes [J]. Zhongguo Dianji Gongcheng Xuebao, 2006, 17 (112-116):
- [44] OVERALL COOLING EFFECTIVENESS ON A FLAT PLATE WITH BOTH FILM COOLING AND IMPINGEMENT COOLING IN HOT GAS CONDITION [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5A, 2016,
- [46] BEHAVIOR OF TEMPERATURE-VELOCITY FLUCTUATIONS AND TURBULENT PRANDTL NUMBER IN DEVELOPING THERMAL TURBULENT BOUNDARY-LAYER ON A FLAT PLATE [J]. BULLETIN OF THE JSME-JAPAN SOCIETY OF MECHANICAL ENGINEERS, 1974, 17 (105): : 351 - 358
- [47] Lateral Edge Effects on the Sherwood Number in Turbulent Flow Over a Flat Plate [J]. JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 140 (02):
- [49] WALL TEMPERATURE AND PRANDTL NUMBER EFFECTS ON TURBULENT BOUNDARY LAYER THICKNESSES AND SHAPE FACTORS FOR SUBSONIC COMPRESSIBLE GAS FLOW OVER A FLAT PLATE [J]. JOURNAL OF ENGINEERING FOR POWER, 1969, 91 (04): : 281 - &