2022
DOI: 10.1016/j.applthermaleng.2022.118792
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Coupled heat transfer analysis of internal and film cooling of turbine blade under medium temperature conditions

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Cited by 21 publications
(5 citation statements)
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“…In addition, the temperature distribution in the airstream field is an important part of melt-blowing, and the exchange of thermal energy in the flow field must be considered. The basic equations of the mathematical model of the meltblown airstream field are thus the mass equation, momentum equation, energy equation, turbulent kinetic energy equation, and specific dissipation rate equation. ,, …”
Section: Modeling and Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…In addition, the temperature distribution in the airstream field is an important part of melt-blowing, and the exchange of thermal energy in the flow field must be considered. The basic equations of the mathematical model of the meltblown airstream field are thus the mass equation, momentum equation, energy equation, turbulent kinetic energy equation, and specific dissipation rate equation. ,, …”
Section: Modeling and Methodsmentioning
confidence: 99%
“…The basic equations of the mathematical model of the meltblown airstream field are thus the mass equation, momentum equation, energy equation, turbulent kinetic energy equation, and specific dissipation rate equation. 35 , 38 , 39 …”
Section: Modeling and Methodsmentioning
confidence: 99%
“…The gas turbine cooling system [27,28] is a multivariable, strongly coupled and nonlinear complex system. From the perspective of the safety of production, the gas turbine cooling automatic control system can avoid the injury of operators caused by manual control, improve the working environment and ensure a smooth production.…”
Section: Gas Turbine Cooling Systemmentioning
confidence: 99%
“…The turbine blade is a core component of the turbine unit used in thermal power stations, and it plays an important role in converting the kinetic energy of high-temperature steam into mechanical energy [1,2]. As turbine blades are in a water-rich environment under high temperature, pressure, and rotational speed for a long time, they are prone to damage or even fracture [3,4], and general metals and composites cannot meet these working requirements. Some nickel-based single-crystal high-temperature alloys, however, have excellent hightemperature strength, oxidation resistance, and thermal corrosion resistance [5,6], enabling them to maintain excellent service performance in high-temperature environments and, hence, be used in aero-engine blades and turbine blades.…”
Section: Introductionmentioning
confidence: 99%