唐豪杰,孙鑫强．发电燃气轮机效率分析及提高措施[J]．燃气轮机技术,2007,20(4)：19-24．Tang Haojie,Sun Xinqiang．Gas turbine power generation efficiency analysis and improving measures[J]．Gas Turbine Technology,2007,20(4)：19-24(in Chinese)．
[2]
Han J C．Influence of unsteady wake on heat transfer coefficients from a gas turbine blade[J]．ASME Tournal of Heat Transfer,1993,115(4)：904-911．
[3]
Womack K M,Volino R J,Schultz M P．Measurment in film cooling flows with periodic wake[J]．Journal of Turbomachinery,2008,130(4)：1008-1017．
[4]
Ekkad S V,Mehendale A B,Han J C．Combined effect of grid turbulence and unsteady wake on film effectiveness and heat transfer coefficient of a gas turbine blade with air and CO 2 film injection[J]．Journal of Turbomachinery,1997,119(7)：594-600．
[5]
Ou S,Han J-C,Mehendale A B．Unsteady wake over a linear turbine blade cascade with air and CO 2 film injection：partⅠ-effect on heat transfer coefficients[J]．Journal of Turbomachinery,1994,116(10)：721-729．
[6]
Shuye Teng,Dong Kee Sohn,Je-Chin Han．Unsteady wake effect on film temperature and effectiveness distributions for a gas turbine blade[J]．Journal of Turbomachinery,2000,122(10)：340-347．
[7]
Arhari R S,Epstein A H．An experiment of film cooling in a rotating transonic turbine[J]．Journal of Turbomachinery,1994,116(10)：63~70．
[8]
Montomoli F,Massini M,Adami P．Effect of incidence angle with wake passing on a film cooled leading edge：a numerical study[J]．International Journal for Numerical Methods in Fluids,2010,63(12)：1359-1374．
[9]
蒋雪辉,赵晓路．非定常尾迹对叶栅气膜冷却效率的影响[J]．推进技术,2004,25(4)：311-315．Jiang Xuehui,Zhao Xiaolu．Effect of unsteady wake on linear cascade film cooling efficiency[J]．Journal of Propulsion Technology,2004,25(4)：311-315(in Chinese)．
[10]
蒋雪辉,赵晓路．非定常尾迹对气膜冷却影响的数值研究[J]．工程热物理学报,2005,26(2)：322-324．Jiang Xuehui,Zhao Xiaolu．Numerical simulation of the unsteady wakes effects on film cooling[J]．Journal of Engineering Thermophysics,2005,26(2)：322-324(in Chinese)．
[11]
袁锋,竺晓程,杜朝辉．尾迹对气膜冷却影响的三维非定常数值模拟[J]．动力工程,2006,26(6)：818-821．Yuan Feng,Zhu Xiaocheng,Du Zhaohui．Three dimensional unsteady numerical simulation of the effect of wakes on film cooling[J]．Journal of Power Engineering,2006,26(6)：818-821(in Chinese)．
[12]
袁锋,张才稳,黄海舟,等．尾迹对涡轮动叶气膜冷却三维非定常数值模拟[J]．热能动力工程,2011,26(5)：507-512．Yuan Feng,Zhang Caiwen,Huang Haizhou,et al．Three dimensional unsteady numerical simulation of the effect of wakes on rotor blade film cooling[J]．Journal of Engineering for Thermal Energy and Power,2011,26(5)：507-512(in Chinese)．
[13]
郭婷婷,张玲,邹晓辉,等．旋转叶片气膜冷却效果的数值研究[J]．中国电机工程学报,2008,28(29)：83-87．Guo Tingting,Zhang Ling,Zou Xiaohui,et al．Numerical study on the film cooling effect of rotating blades[J]．Proceedings of the CSEE,2008,28(29)：83-87(in Chinese)．
[14]
李少华,吕敏,张玲,等．非定常尾迹及其对动叶气膜冷却影响的数值研究[J]．动力工程学报,2011,31(12)：922-927．Li Shaohua,Lü Min,Zhang Ling,et al．Numerical simulation of unsteady wakes and the influence on film-cooling effectiveness[J]．Journal of Chinese Society of Power Engineering,2011,31(12)：922-927(in Chinese)．
[15]
李少华,李知骏,曲宏伟,等．非定常尾迹对动叶气膜冷却影响的数值模拟[J]．电站系统工程,2011,27(1)：3-5．Li Shaohua,Li Zhijun,Qu Hongwei,et al．Numerical simulation study on the effect of unsteady wakes on leading edge film cooling[J]．Power System Engineering,2011,27(1)：3-5(in Chinese)．
[16]
李少华,王成荫,吴殿文,等．非定常尾迹对叶栅温度影响的数值研究[J]．东北电力大学学报,2010,30(2)：1-5．Li Shaohua,Wang Chengyin,Wu Dianwen,et al．Numerical prediction of the temperature of first grade cascade on the effects of unsteady wakes[J]．Journal of Northeast Dianli University,2010,30(2)：1-5(in Chinese)．
[17]
周莉,张鑫,蔡元虎．非定常尾迹宽度对动叶气膜冷却效果的影响[J]．中国电机工程学报,2011,31(29)：97-102．Zhou Li,Zhang Xin,Cai Yuanhu．Effect of unsteady wake width on the film-cooling effectiveness for a gas turbine blade[J]．Proceeding of the CSEE,2011,31(29)：97-102(in Chinese)．
[18]
周莉,韦威,蔡元虎．非定常尾迹输运对动叶气膜流场影响[J]．航空动力学报,2012,27(8)：1696-1703． Zhou Li,Wei Wei,Cai Yuanhu．Effect of unsteady transportation on film cooling flowfield of rotating turbine blade[J]．Journal of Aerospace Power,2012,27(8)：1696-1703(in Chinese)．
[19]
周莉,张鑫,蔡元虎．非定常环境下动叶气膜冷却流场的数值模拟[J]．航空动力学报,2011,26(8)：1695-1701．Zhou Li,Zhang Xin,Cai Yuanhu．Unsteady numerical simulation of the turbine blade film cooling[J]．Journal of Aerospace Power,2011,26(8)：1695-1701(in Chinese)．
[20]
Yamamoto．Production and development of secondary flows and losses in two types of straight turbine cascades：part 2-A rotor case[J]．Journal of Turbomachinery,1987,109(4)：194-200．
[21]
Schulte V,Hodson H P．Wake-separation bubble interaction in Low Pressure Turbines[C]//30th Aerospace Sciences Meeting and Exhibit,Indianapolis,Indiana,USA,1994．
[22]
Volker S,Howard P H．Unsteady wake-induced boundary layer transition in high lift LP turbines[C]//Proceeding of the 1996 International Gas Turbine and Aeroengine Congress & Exhibition,Burminghan,UK,1996．
[23]
杨汇涛,曹玉璋．旋转叶片端部气膜冷却的数值计算[J]．航空动力学报,1998,13(3)：285-289．Yang Huitao,Cao Yuzhang．Endwall film-cooling of rotated blade[J]．Journal of Aerospace Power,1998,13(3)：285-289(in Chinese)．
[24]
韩介勤,桑地普·杜达,斯瑞纳斯·艾卡德．燃气轮机传热和冷却技术[M]．西安：西安交通大学出版社,2005,20-134．Je-Chin Han,Sandip Dutta,Srinath V Ekkad．Gas turbine heat transfer and cooling technology[M]．Xi’an：Xi’an Jiaotong University Press,2005,20-134(in Chinese)．
