| 1 |
Influence of flat endwall simplification in gas turbines on cooling performance
Yao R, Wang JH, Wang M, Wang L
International Journal of Heat and Mass Transfer, 130, 1226, 2019 |
| 2 |
Numerical evaluation of heat/mass transfer analogy for leading edge showerhead film cooling on a first-stage vane
Ravelli S, Barigozzi G
International Journal of Heat and Mass Transfer, 129, 842, 2019 |
| 3 |
Effect of blockage configuration on film cooling with and without mist injection
Tian K, Wang J, Liu C, Yang L, Sunden B
Energy, 153, 661, 2018 |
| 4 |
Simultaneous kHz-rate temperature and velocity field measurements in the flow emanating from angled and trenched film cooling holes
Schreivogel P, Abram C, Fond B, Strausswald M, Beyrau F, Pfitzner M
International Journal of Heat and Mass Transfer, 103, 390, 2016 |
| 5 |
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 |
| 6 |
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 |
