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Prapamonth... [6]
杨国伟 [6]
孙振旭 [3]
银波 [3]
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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)
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View/Download:293/94
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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)
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View/Download:435/110
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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)
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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)
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View/Download:341/90
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Submit date:2020/05/18
Computational fluid dynamics
Drag reduction
Supersonic flow
Energy deposition
Opposing jet
Analysis of Aerodynamic Noise Characteristics of High-Speed Train Pantograph with Different Installation Bases
期刊论文
APPLIED SCIENCES-BASEL, 2019, 卷号: 9, 期号: 11, 页码: 21
Authors:
Yao YF(姚永芳)
;
Sun ZX(孙振旭)
;
Yang GW(杨国伟)
;
Prapamonthon P
View
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Adobe PDF(10233Kb)
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View/Download:263/59
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Submit date:2019/09/09
high-speed train
pantograph
aerodynamic noise
large eddy simulation
acoustic finite element method
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)
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View/Download:178/67
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Submit date:2020/11/20
Aerothermal condition
Cooling effectiveness
Cooling performance
Thermal sensitivity
Turbine vane