| 1 |
Influences of effusion hole diameter on impingement/effusion cooling performance at turbine blade leading edge
Zhou JF, Wang XJ, Li J
International Journal of Heat and Mass Transfer, 134, 1101, 2019 |
| 2 |
Effects of film cooling hole locations on flow and heat transfer characteristics of impingement/effusion cooling at turbine blade leading edge
Zhou JF, Wang XJ, Li J, Li YD
International Journal of Heat and Mass Transfer, 126, 192, 2018 |
| 3 |
Development of a propeller-type hollow micro-hydraulic turbine with excellent performance in passing foreign matter
Uchiyama T, Honda S, Degawa T
Renewable Energy, 126, 545, 2018 |
| 4 |
Numerical simulation on film cooling with compound angle of blade leading edge model for gas turbine
Gao WJ, Yue ZF, Li L, Zhao ZN, Tong FJ
International Journal of Heat and Mass Transfer, 115, 839, 2017 |
| 5 |
Numerical study on the effect of jet nozzle aspect ratio and jet angle on swirl cooling in a model of a turbine blade leading edge cooling passage
Liu Z, Li J, Feng ZP, Simon T
International Journal of Heat and Mass Transfer, 90, 986, 2015 |
| 6 |
Experimental investigation on the leading edge film cooling of cylindrical and laid-back holes with different hole pitches
Liu CL, Zhu HR, Zhang ZW, Xu DC
International Journal of Heat and Mass Transfer, 55(23-24), 6832, 2012 |
| 7 |
Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine blade leading edge
Liu Z, Feng ZP
International Journal of Heat and Mass Transfer, 54(23-24), 4949, 2011 |
| 8 |
Numerical study of film cooled rotor leading edge with tip clearance in 1-1/2 turbine stage
Yang HT, Chen HC, Han JC, Moon HK
International Journal of Heat and Mass Transfer, 51(11-12), 3066, 2008 |
| 9 |
Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes
Ahn J, Schobeiri MT, Han JC, Moon HK
International Journal of Heat and Mass Transfer, 50(1-2), 15, 2007 |
