| Citation: | JIA Guang-sen, ZHANG Li, LU Cong-ming, LUO Jian-xia, HUANG Xiao-yang. Film cooling performance with internal coolant channel crossflow[J]. Journal of Aerospace Power, 2015, 30(4): 823-830. doi: 10.13224/j.cnki.jasp.2015.04.008 |
| [1] |
倪萌, 朱惠人, 裘云, 等.航空发动机涡轮叶片冷却技术综述[J].燃气轮机技术, 2005, 18(4):24-38. NI Meng, ZHU Huiren, QIU Yun, et al.Review of aero-turbine blade cooling technologies[J].Gas Turbine Technology, 2005, 18(4):24-38.(in Chinese)
|
| [2] |
Goldstein R J.Film cooling[J].Advances in Heat Transfer, 1971, 7(1):321-379.
|
| [3] |
Goldstein R J, Eckert E R G, Burggraf F.Effects of hole geometry and density on three-dimensional film cooling[J].International Journal of Heat and Mass Transfer, 1974, 17(5):595-607.
|
| [4] |
Bunker R S.A review of shaped hole turbine film-cooling technology[J].Journal of Heat Transfer, 2005, 127(4):441-453.
|
| [5] |
Bogard D G, Thole K A.Gas turbine film cooling[J]. Journal of Propulsion and Power, 2006, 22(2):249-270.
|
| [6] |
Lutum E, Johnson B V.Influence of the hole length-to-diameter ratio on film cooling with cylindrical holes[J].Journal of Turbomachinery, 1999, 121(2):209-216.
|
| [7] |
Hay N, Lampard D, Benmansour S.Effect of crossflows on the discharge coefficient of film cooling holes[J].Journal for Engineering for Power, 1983, 105(2):243-248.
|
| [8] |
Gritsch M, Saumweber C, Schulz A, et al.Effect of internal coolant crossflow orientation on the discharge coefficient of shaped film-cooling holes[J].Journal of Turbomachinery, 2000, 122(1):146-152.
|
| [9] |
Thole K A, Gritsch M, Schulz A, et al.Effect of a crossflow at the entrance to a film-cooling hole[J].Journal of Fluids Engineering, 1997, 119(3):533-540.
|
| [10] |
白江涛, 朱惠人, 刘存良.内通道交错横流对气膜冷却效率的影响[J].航空动力学报, 2008, 23(8):1353-1358. BAI Jiangtao, ZHU Huiren, LIU Cunliang.Numerical study the effect of internal coolant crossflow on film cooling effectiveness[J].Journal of Aerospace Power, 2008, 23(8):1353-1358.(in Chinese)
|
| [11] |
李春林, 朱惠人, 杜小琴, 等.内冷通道特性对外表面气膜冷却换热影响研究[J].汽轮机技术, 2009, 51(5):357-360. LI Chunlin, ZHU Huiren, DU Xiaoqin, et al.The effect of internal cooling channel on the heat transfer of outer surface film cooling[J].Turbine Technology, 2009, 51(5):357-360.(in Chinese)
|
| [12] |
刘存良, 朱惠人, 白江涛, 等.基于瞬态液晶测量技术的收缩扩张形孔气膜冷却特性[J].航空学报, 2009, 30(5):812-818. LIU Cunliang, ZHU Huiren, BAI Jiangtao, et al.Film cooling characteristics of converging-expanding hole with transient liquid crystal measurement technique[J].Acta Aeronautica et Astronautica Sinica, 2009, 30(5):812-818.(in Chinese)
|
| [13] |
Drost U, Bolcs A, Hoffs A.Utilization of the transient liquid crystal technique for film cooling effectiveness and heat transfer investigations on a flat plate and a turbine airfoil[R].Orlando:ASME International Gas Turbine and Aeroengine Congress and Exhibition, 1997.
|
| [14] |
Yan Y, Owen J M.Uncertainties in transient heat transfer measurements with liquid crystal[J].International Journal of Heat and Fluid Flow, 2002, 23(1):29-35.
|
| [15] |
York W D, Leylek J H.Leading-edge film-cooling physics:Part Ⅰ adiabatic effectiveness[R].Amsterdam, Netherlands:ASME Turbo Expo 2002, Power for Land, Sea, and Air, 2002.
|
| [16] |
Na S, Zhu B, Bryden M, et al.CFD analysis of film cooling[R].AIAA-2006-0022, 2006.
|
| [17] |
刘存良.新型高效气膜孔冷却特性研究[D].西安:西北工业大学, 2009. LIU Cunliang.Research on the film cooling characteristics of high-performance shaped film holes[D].Xi'an:Northwestern Polytechnical University, 2009.(in Chinese)
|
| [18] |
Walters D K, Leylek J H.A detailed analysis of film-cooling physics:Part Ⅰ streamwise injection with cylindrical holes[J].Journal of Turbomachinery, 2000, 122(1):102-112.
|