| 雷诺数对大涵道比涡扇发动机性能的影响仿真 |
| |
| 引用本文： | 赵运生,胡骏,屠宝锋,王志强.雷诺数对大涵道比涡扇发动机性能的影响仿真[J].中国机械工程,2013,24(21):2867-2871. |
| |
| 作者姓名： | 赵运生 胡骏 屠宝锋 王志强 |
| |
| 作者单位： | 南京航空航天大学,南京,210016 |
| |
| 基金项目： | 高等学校博士学科点专项科研基金资助项目（20113218120006）
Research Fund for the Doctoral Program of Higher Education of China（No. 20113218120006） |
| |
| 摘 要： | 为了评估雷诺数对某大涵道比涡扇发动机的影响,利用Wassell等修正方法,对发动机主要部件的特性进行了雷诺数修正,并利用发展的性能仿真程序进行计算和对比。结果表明,在高空低马赫数下,雷诺数对大涵道比涡扇发动机性能影响较大,造成发动机的推力减小约1.98%、耗油率增大约3.04%,同时影响发动机的喘振边界及共同工作线,降低其可用稳定裕度。
|
| 关 键 词： | 雷诺数 涡扇发动机 数值仿真 大涵道比 性能 |
Simulation of Reynolds Number's Effect on Performance of High Bypass Ratio Turbofan |
| |
| Zhao Yunsheng,Hu Jun,Tu Baofeng,Wang Zhiqiang.Simulation of Reynolds Number's Effect on Performance of High Bypass Ratio Turbofan[J].China Mechanical Engineering,2013,24(21):2867-2871. |
| |
| Authors: | Zhao Yunsheng Hu Jun Tu Baofeng Wang Zhiqiang |
| |
| Affiliation: | Nanjing University of Aeronautics and Astronautics,Nanjing,210016 |
| |
| Abstract: | For assessing the Reynolds number's effect
on a high bypass ratio turbofan,the correction methods such as Wassell were used for
the main component characteristics,and cooperated with a new performance program to simulate
the effects of Reynolds number on engine's performance.
Results show that Reynolds number has grievous effects on the turbofan in high flight and low
Mach number region,the thrust is declined by near 1.98%,the specific fuel consumption
is escalated by near 3.04%,the stall lines and operating lines are affected and the stall margin
is declined as well. |
| |
| Keywords: | Reynolds number turbofan simulation high bypass ratio performance |
|
| 点击此处可从《中国机械工程》浏览原始摘要信息 |
|
点击此处可从《中国机械工程》下载全文 |
|
