| Citation: | LUO Guo-liang, YANG Wei-hua, CAO Jun, SHI Rui, SONG Shuang-wen. Experimental study of discharge coefficient and cooling effectiveness for impingement effusion cooling in curved section[J]. Journal of Aerospace Power, 2011, 26(8): 1688-1694.
|
| [1] |
Lefebvre A H.Gas turbine combustion[M].New York:Hemisphere Publishing Corporation,1983.
|
| [2] |
Meller A M.Design of modern turbine combustor[M].New York:Academic Press Inc.,1990.
|
| [3] |
Choe H,Kay W M,Mlffat R J.Turbulent boundary layer on a full-coverage film-cooled surface-an experimental heat transfer study with normal injection.Stanford,California:Report HMT-22,Department of Mechanical Engineering,Stanford University,1973.
|
| [4] |
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)
|
| [5] |
Al Dabagh A M,Andrews G E,Husain R A A A,et al.Impingement/effusion cooling:the influence of the number of impingement holes and pressure loss on the heat transfer coefficient.ASME Paper No.89-GT-188,1989.
|
| [6] |
Andrews G E,Asere A A,Hussain C I,et al.Transpiration and impingement/effusion cooling of gas turbine combustion chambers.ISABE 85-7095,1985.
|
| [7] |
许全宏,林宇震,刘高恩.冲击加多斜孔双层壁冷却方式冲击换热系数[J].大连理工大学学报,2001,41(suppl.):63-66. XU Quanhong,LIN Yuzhen,LIU Gaoen.Heat transfer coefficient of impingement/effusion double wall cooling method[J].Journal of Dalian University of Technology,2001,41(suppl.):63-66.(in Chinese)
|
| [8] |
Myers G.Comparison of advanced cooling concepts using color thermography.AIAA 85-1289,1985.
|
| [9] |
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)
|
| [10] |
Wassell A B.The development and application of improved combustor wall cooling techniques.ASME 80-GT-66,1980.
|
| [11] |
Nealy D A.Evalution of laminated porous wall materials for combustor liner cooling.ASME 79-GT-100,1979.
|
| [12] |
李彬.冲击-致密微孔浮动壁火焰筒冷却研究.南京:南京航空航天大学,2008. LI Bin.Investigation of impingement/effusion float-wall cooling of flam tube.Nanjing:Nanjing University of Aeronautics and Astronautics,2008.(in Chinese)
|
| [13] |
张驰,赵梦梦,林宇震,等.弯曲壁上开孔倾角对气膜孔流量系数的影响[J].航空动力学报,2007,22(7):1127-1131. ZHANG Chi,ZHAO Mengmeng,LIN Yuzhen,et al.Effect of inclined angle on discharge coefficient of the discrete holes in curved wall[J].Journal of Aerospace Power,2007,22(7):1127-1131.(in Chinese)
|
| [14] |
王利.火焰筒壁面复合冷却结构的流动与换热特性研究.南京:南京航空航天大学,2010. WHANG Li.Investigation on flow and heat transfer characteristics in compound cooling configuration of chamber wall.Nanjing:Nanjing University of Aeronautics and Astronautics,2010.(in Chinese)
|
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