| 1 |
Experimental investigation on the effects of rotation and the blowing ratio on the leading-edge film cooling of a twist turbine blade
Li HW, Han F, Ma YW, Wang HC, Zhou ZY, Tao Z
International Journal of Heat and Mass Transfer, 129, 47, 2019 |
| 2 |
Effects of design parameters on aerodynamic performance of a counter-rotating wind turbine
Lee S, Kim H, Son E, Lee S
Renewable Energy, 42, 140, 2012 |
| 3 |
Application of the TLVA model for predicting film cooling under rotating frames
Xu GQ, Zhu JQ, Tao Z
International Journal of Heat and Mass Transfer, 53(15-16), 3013, 2010 |
| 4 |
Suitability of three different two-equation turbulence models in predicting film cooling performance over a rotating blade
Tao Z, Zhao ZM, Ding ST, Xu GQ, Wu HW
International Journal of Heat and Mass Transfer, 52(5-6), 1268, 2009 |
| 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 |
| 7 |
Temperature distributions in rotary-blade coupling of a 4WD vehicle with longitudinal ribbed turbulators
Yeh JP, Tzeng SC, Tseng HC
Applied Energy, 80(2), 155, 2005 |
