검색결과 : 7건
| No. | Article |
|---|---|
| 1 |
Turbine platform phantom cooling from airfoil film coolant, with purge flow Yang X, Liu Z, Liu ZS, Feng ZP, Simon T International Journal of Heat and Mass Transfer, 140, 25, 2019 |
| 2 |
Experimental and numerical study on the effects of rib orientation angle on film cooling performance of compound angle holes Ye L, Liu CL, Liu HY, Zhu HR, Luo JX International Journal of Heat and Mass Transfer, 126, 1099, 2018 |
| 3 |
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 |
| 4 |
Effects of compound angle on film cooling effectiveness with different streamwise pressure gradient and convex curvature Qin YM, Li XY, Ren J, Jiang HD International Journal of Heat and Mass Transfer, 86, 482, 2015 |
| 5 |
Internal wall-jet film cooling with compound angle cylindrical holes Shine SR, Kumar SS, Suresh BN Energy Conversion and Management, 68, 54, 2013 |
| 6 |
Effects of pressure gradient on film cooling effectiveness from two rows of simple and compound angle holes in combination Maiteh BY, Jubran BA Energy Conversion and Management, 45(9-10), 1457, 2004 |
| 7 |
Heat-Transfer - A Review of 1994 Literature Eckert ER, Goldstein RJ, Ibele WE, Patankar SV, Simon TW, Strykowski PJ, Tamma KK, Kuehn TH, Barcohen A, Heberlein JV, Hofeldt DL, Davidson JH, Bischof J, Kulacki F International Journal of Heat and Mass Transfer, 40(16), 3729, 1997 |