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| Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
Authors: Ju SJ(鞠胜军); Sun ZX(孙振旭) ; Yang GW(杨国伟); Prapamonthon P; Zhang JY
 Adobe PDF(3818Kb) |  Favorite | View/Download：452/117 | Submit date：2020/11/30
Optimization design Drag reduction Supersonic flow Energy deposition Opposing jet |
| Separate and Combined Effects of Surface Roughness and Thermal Barrier Coating on Vane Cooling Performance 期刊论文
JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS, 2020, 卷号: 12, 期号: 5, 页码: 15
Authors: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH
Adobe PDF(2963Kb) | Favorite | View/Download：345/123 | Submit date：2020/11/30
gas-turbine heat transfer surface roughness cooling performance thermal barrier coating |
| Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
Authors: Ju SJ; Sun ZX(孙振旭); Yang GW(杨国伟); Prapamonthon P; Zhang JY
Adobe PDF(3216Kb) | Favorite | View/Download：360/95 | Submit date：2020/05/18
Computational fluid dynamics Drag reduction Supersonic flow Energy deposition Opposing jet |
| Understanding of temperature and cooling effectiveness sensitivity of a film-cooled vane under coolant inlet temperature effect: A case study 期刊论文
CASE STUDIES IN THERMAL ENGINEERING, 2019, 卷号: 14, 页码: UNSP 100505
Authors: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH
Adobe PDF(3342Kb) | Favorite | View/Download：265/81 | Submit date：2020/03/21
TURBINE BLADE HEAT-TRANSFER |
| CHT/CFD Analysis of Thermal Sensitivity of a Transonic Film-Cooled Guide Vane 期刊论文
CMES-COMPUTER MODELING IN ENGINEERING & SCIENCES, 2019, 卷号: 119, 期号: 3, 页码: 593-615
Authors: Prapamonthon P; Yooyen S; Sleesongsom S
Adobe PDF(3354Kb) | Favorite | View/Download：320/75 | Submit date：2019/09/09
Conjugate heat transfer film cooling thermal sensitivity |
| Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions 会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
Authors: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH(张莫晗)
Adobe PDF(2782Kb) | Favorite | View/Download：206/74 | Submit date：2020/11/20
Aerothermal condition Cooling effectiveness Cooling performance Thermal sensitivity Turbine vane |
| Investigation of Cooling Performances of a Non-Film-Cooled Turbine Vane Coated with a Thermal Barrier Coating Using Conjugate Heat Transfer 期刊论文
ENERGIES, 2018, 卷号: 11, 期号: 4
Authors: Prapamonthon P; Yooyen S; Sleesongsom S; Dipasquale D; Xu HZ; Wang JH; Ke ZQ
Adobe PDF(64361Kb) | Favorite | View/Download：436/42 | Submit date：2018/07/17
Turbine Vane Heat Transfer Coefficient Thermal Barrier Coating Turbulence Intensity Conjugate Heat Transfer |
