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| Parametric study on wing-lambda-shock formation 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
Authors: Chainok S; Rungroch T; Chairach P; Prapamonthon P; Yooyen S; Yin B(银波) ; Yang GW(杨国伟); Ju SJ(鞠胜军)
 Adobe PDF(3026Kb) |  Favorite | View/Download：295/94 | Submit date：2021/11/30
Shock Supersonic flow Transonic flow |
| 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：437/111 | 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：326/114 | Submit date：2020/11/30
gas-turbine heat transfer surface roughness cooling performance thermal barrier coating |
| Recent progress in flexibility effects on wing aerodynamics and acoustics 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2020, 页码: 37
Authors: Prapamonthon P; Yin B(银波); Yang GW(杨国伟); Zhang MH(张莫晗); Lu PP(卢盼盼)
Adobe PDF(3624Kb) | Favorite | View/Download：377/218 | Submit date：2020/08/26
Flexibility wing lift propulsion acoustics |
| 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：344/90 | 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
 View | Adobe PDF(3342Kb) | Favorite | View/Download：196/67 | Submit date：2020/03/21
TURBINE BLADE HEAT-TRANSFER |
| 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
View | Adobe PDF(3342Kb) | Favorite | View/Download：250/77 | Submit date：2020/03/21
TURBINE BLADE HEAT-TRANSFER |
| 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：180/69 | Submit date：2020/11/20
Aerothermal condition Cooling effectiveness Cooling performance Thermal sensitivity Turbine vane |
