| Citation: | Numerical computation and analysis of impingement/effusion cooling performance on concave wall[J]. Journal of Aerospace Power, 2017, 32(11): 2561-2567. doi: 10.13224/j.cnki.jasp.2017.11.001 |
| [1] |
方昌德.世界航空发动机手册[M].北京:航空工业出版社,1996.
|
| [2] |
MELLER A M.Design of modern turbine combustor[M].New York:Academic Press Incorporated,1990.
|
| [3] |
LEFEBVRE A H.Gas turbine combustion[M].New York:Hemisphere Publishing Corporation,1983.
|
| [4] |
AL DABAGH A M,ANDREWS G E,ABDUL HUSAIN R A A,et al.Impingement/effusion cooling:the influence of the number of impingement holes and pressure loss on the heat transfer coefficient[R].ASME Paper 89-GT-188,1989.
|
| [5] |
ANDREWS G E,ASERE A A,HUSSAIN C I,et al.Transpiration and impingement/effusion cooling of gas turbine combustion chambers[R].ISABE 85-7095,1985.
|
| [6] |
胡超,许全宏,徐剑,等.冲击/发散冷却壁温分布和冷却效率研究[J].航空动力学报,2008,23(10):1800-1804.HU Chao,XU Quanhong,XU Jian,et al.Investigation of the wall temperature distribution and cooling efficiency for impingement/effusion cooling scheme[J].Journal of Aerospace Power,2008,23(10):1800-1804.(in Chinese)
|
| [7] |
俞文利,林宇震,刘高恩.冲击加多斜孔双层壁冷却方式多斜孔内换热研究[J].航空动力学报,2001,16(4):365-369.YU Wenli,LIN Yuzhen,LIU Gaoen.Investigation of heat transfer inside inclined multihole in the impingement/inclined multihole double wall[J].Journal of Aerospace Power,2001,16(4):365-369.(in Chinese)
|
| [8] |
许全宏,林宇震,刘高恩.冲击/发散复合冷却方式发散壁热侧换热系数的研究[J].航空动力学报,2004,19(2):213-218.XU Quanhong,LIN Yuzhen,LIU Gaoen.Study of the effusion wall film heat transfer coefficients of impingement/effusion double wall cooling method[J].Journal of Aerospace Power,2004,19(2):213-218.(in Chinese)
|
| [9] |
许全宏,林宇震,刘高恩.冲击加多斜孔双层壁冷却方式流量系数研究[J].推进技术,2000,21(5):49-52.XU Quanhong,LIN Yuzhen,LIU Gaoen.Discharge coefficient of double wall with discrete hole and inclined multihole for combustor liner[J].Journal of Propulsion Technology,2000,21(5):49-52.(in Chinese)
|
| [10] |
王磊,张靖周,杨卫华,等.冲击/发散冷却气膜冷却效率的实验研究[J].工程热物理学报,2007,28(2):97-100.WANG Lei,ZHANG Jingzhou,YANG Weihua,et al.Experiment research on film cooling effectiveness of impingement/effusion cooling[J].Journal of Engineering Thermophysics,2007,28(2):97-100.(in Chinese)
|
| [11] |
罗国良,杨卫华,曹俊,等.弯曲段壁面冲击发散冷却结构流量系数与冷却效率的实验[J].航空动力学报,2011,26(8):1687-1694.LUO Guoliang,YANG Weihua,CAO Jun,et al.Experimental study of discharge coefficient and cooling effectiveness for impingement effusion cooling in curved section[J].Journal of Aerospace Power,2011,26(8):1687-1694.(in Chinese)
|
| [12] |
曹俊,杨卫华,石蕊,等.弯曲段壁面冲击发散冷却效率的实验[J].推进技术,2011,32(4):479-484.CAO Jun,YANG Weihua,SHI Rui,et al.Film cooling effectiveness experiment of impingement effusion cooling in curved section[J].Journal of Propulsion Technology,2011,32(4):479-484.(in Chinese)
|
| [13] |
WASSELL A B.The development and application of improved combustor wall cooling techniques[R].ASME Paper 80-GT-66,1980.
|
| [14] |
林宇震,俞文利,刘高恩,等.冲击加发散双层壁冷却方式压降分配对斜孔内对流换热影响的研究[J].航空学报,2003,24(2):97-101.LIN Yuzhen,YU Wenli,LIU Gaoen,et al.Influence of pressure drop distribution on the convection heat transfer inside the inclined hole of impingement/effusion cooling[J].Acta Aeronautica et Astronautica Sinica,2003,24(2):97-101.(in Chinese)
|
| [15] |
俞文利.冲击/发散冷却方式多斜孔内换热及优化研究[D].北京:北京航空航天大学,2001.YU Wenli.The heat transfer study on impingement/effusion cooling and optimum design for combustor liner[D].Beijing:Beijing University of Aeronautics and Astronautics,2001.(in Chinese)
|
| [16] |
唐庆如.冲击加多斜孔双层壁对流与冲击换热优化研究[J].航空动力学报,2007,22(3):375-379.TANG Qingru.A study of optimization of convection and heat transfer of impingement/effusion double wall[J].Journal of Aerospace Power,2007,22(3):375-379.(in Chinese)
|
| [17] |
王梅娟,彭剑勇,严明超,等.冲击+发散冷却传热特性的试验研究[C]∥中国航空学会第十六届燃烧与传热传质学术交流会论文集.北京:中国航空学会,2001:563-569.
|
| [18] |
HARRINGTON M K,MCWATERS M A,BOGARD D G,et al.Full coverage film cooling with short normal injection holes[R].ASME Paper 2001-GT-0130,2001.
|