| Citation: | LING Dai-jun, WANG Hui, MA Chang-you. Subsonic compressor plane cascade experiment at low Reynolds number[J]. Journal of Aerospace Power, 2013, 28(1): 171-179.
|
| [1] |
胡晓煜.国外高空长航时无人机动力技术的发展[J].燃气涡轮试验与研究,2006,19(4):56-60. HU Xiaoyu.Development of high altitude long endurance UAV propulsion technology[J].Gas Turbine Experiment and Research,2006,19(4):56-60.(in Chinese)
|
| [2] |
屠秋野,陈玉春,苏三买,等.雷诺数对高空长航时无人机发动机调节计划和性能影响[J].推进技术,2005,26(2):125-128. TU Qiuye,CHEN Yuchun,SU Sanmai,et al.Effects of Reynolds number on control schedule and performance of HALE engine[J].Journal of Propulsion Technology,2005,26(2):125-128.(in Chinese)
|
| [3] |
王进,骆广琦,陶增元.雷诺数对压气机特性及发动机稳定性影响的计算和分析[J].航空动力学报,2003,18(1):20-23. WANG Jin,LUO Guangqi,TAO Zengyuan.Effects of Reynolds number on compressor performance and engine stability[J].Journal of Aerospace Power,2003,18(1):20-23.(in Chinese)
|
| [4] |
Lake J P,King P I,Rivir R B.Reduction of separation losses on a turbine blade with low Reynolds number .AIAA 9920242,1999.
|
| [5] |
Weinberg M,Wyzykowski J .Development and testing of a commerical turbofan engine for high altitude UAV applications .SAE 200120122972,2001.
|
| [6] |
尹泽勇,李上福,李概奇.无人机动力装置的现状与发展[J].航空发动机,2007,33(1):10-15. YIN Zeyong,LI Shangfu,LI Gaiqi.Current state and development of the unmanned aerial vehicle powerplants[J].Aeroengine,2007,33(1):10-15.(in Chinese)
|
| [7] |
夏钦斌,王如根,周敏,等.低雷诺数条件下跨声速转子轴向倾斜缝处理机匣扩稳研究[J].航空动力学报,2010,25(6):1389-1394. XIA Qinbin,WANG Rugen,ZHOU Min,et al.Research on the effects of a transonic compressor rotor with axial skewedslots casing treatment at low Reynolds number[J].Journal of Aerospace Power,2010,25(6):1389-1394.(in Chinese)
|
| [8] |
刘波,侯为民,项效镕.高空低雷诺数二维抗分离叶型研究[J].西北工业大学学报,2008,26(6):703-706. LIU Bo,HOU Weimin,XIANG Xiaorong.Exploring new ideas and new methods in 2D fan-compressor cascade profile optimization design for low Reynolds number and high altitude[J].Journal of North-western Polytechnical University,2008,26(6):703-706.(in Chinese)
|
| [9] |
孙皓,薛志恒,李军,等.低雷诺数对透平叶片间隙泄漏流动影响的研究[J].西安交通大学学报,2010,44(3):11-15. SUN Hao,XUE Zhiheng,LI Jun,et al.Effects of low Reynolds number on turbine blade tip leakage flow[J].Journal of Xi'an Jiaotong University,2010,44(3):11-15.(in Chinese)
|
| [10] |
赵峰,桂幸民.低雷诺数效应对某可控扩散叶型性能的影响[J].航空动力学报,2006,21(2):285-289. ZHAO Feng,GUI Xingmin.The low Reynolds number effects on the performance of some controlled diffusion airfoils[J].Journal of Aerospace Power,2006,21(2):285-289.(in Chinese)
|
| [11] |
伊进宝,乔渭阳.低雷诺数下涡轮叶栅流动分离实验与数值模拟[J].推进技术,2008,29(2):208-213. YI Jinbao,QIAO Weiyang.Experimental and numerical investigation on flow separation in turbine cascade with low Reynolds number[J].Journal of Propulsion Technology,2008,29(2):208-213.(in Chinese)
|
| [12] |
孙大伟,乔渭阳,许开富,等.低雷诺数条件下涡轮性能的计算研究[J].航空动力学报,2008,23(7):1253-1259. SUN Dawei,QIAO Weiyang,XU Kaifu,et al.Study on turbine performance at low Reynolds number[J].Journal of Aerospace Power,2008,23(7):1253-1259.(in Chinese)
|
| [13] |
顾明皓,桂幸民.低雷诺数效应对某型风扇的性能影响及改进方案研究[J].航空动力学报,2004,19(4):438-443. GU Minghao,GUI Xingming.Low Reynolds number effects on the performance of some fans and the modified design[J].Journal of Aerospace Power,2004,19(4):438-443.(in Chinese)
|
| [14] |
王如根,周敏,赵英武,等.跨声速压气机低雷诺数下流动失稳机制研究[J].航空动力学报,2009,24(2):414-419. WANG Rugen,ZHOU Min,ZHAO Yingwu,et al.Research on flow instability mechanism of transonic compressor at low Reynolds number[J].Journal of Aerospace Power,2009,24(2):414-419.(in Chinese)
|
| [15] |
杨琳,冯涛,邹正平,等.低雷诺数涡轮内部流场分析[J].北京航空航天大学学报,2005,31(11):1194-1197. YANG Lin,FENG Tao,ZOU Zhengping,et al.Analysis of turbine flow field under low Reynolds number condition[J].Journal of Beijing University of Aeronautics and Astronautics,2005,31(11):1194-1197.(in Chinese)
|
| [16] |
凌代军,姜正礼,于进涛,等.低雷诺数平面叶栅方法研究[J].燃气涡轮试验与研究,2011,24(3):1-6. LING Daijun,JIANG Zhengli,YU Jingtao,et al.Experimental investigation methods on low Reynolds number plane cascade[J].Gas Turbine Experiment and Research,2011,24(3):1-6.(in Chinese)
|
DownLoad: