期刊文献+

能量法和时域法在叶片颤振计算中的比较研究 被引量:4

Comparative Study on Energy Method and Time- domain Method for Blade Flutter Predictions
下载PDF
导出
摘要 为了对能量法和时域法这两类叶片颤振计算中的代表性方法进行比较研究,分别介绍了基于CFD技术发展的双通道形状修正能量法和CFD/CSD耦合时域法。前者利用傅里叶级数对周向边界流场变量进行修正而相应的系数由内部单元值进行更新。后者通过耦合非定常气动力计算和结构运动方程求解来实现流场和结构场在时域内的推进。对跨声速风扇转子Rotor67进行计算,结果表明两种方法能够给出一致的颤振特性结果,最后结合算例从多方面对它们进行了比较。 A comparative study of two kinds of representative methods for blade flutter predictions energy method and time domain method is presented in this paper.Particularly,two self developed methods were introduced,which are the double passage shape correction (DPSC) method and the computational fluid dynamics/computational structural dynamics (CFD/CSD) coupled time domain method,respectively.For the former one,the main idea was to correct the flow variables at circumferential boundaries through the Fourier series while the corresponding Fourier coefficients were updated from flow variables at interior boundaries.For the latter one,through coupling between the unsteady aerodynamic calculation and the structural dynamic analysis,the flow field and the structural filed were advanced in time accurately and efficiently,and thus the actual vibration response to the structural disturbance could be obtained.By applying these two methods to a transonic fan rotor Rotor67,it was shown that both of them predicted consistent flutter characteristics.Finally,based on the computed results,comprehensive comparisons between these two methods were carried out from several aspects.
作者 周迪 吕彬彬 陆志良 郭同庆 丁力 ZHOU Di;LV Bin-bin;LU Zhi-liang;GUO Tong-qing;DING Li(Key Laboratory of Unsteady Aerodynamics and Flow Control of Ministry of Industry and Information Technology, College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;State Environmental Protection Key Laboratory of Atmospheric Physical Modeling and Pollution Control, State Power Environmental Protection Research Institute,Nanjing 210031,China)
出处 《航空计算技术》 2019年第5期43-48,共6页 Aeronautical Computing Technique
基金 国家自然科学基金项目资助(11872212) 中国博士后基金项目资助(2019M650112) 江苏省高校优势学科建设工程项目资助(PAPD)
关键词 风扇叶片 颤振 计算流体力学 能量法 时域法 fan blade flutter computational fluid dynamics(CFD) energy method time domain method
  • 相关文献

参考文献3

二级参考文献50

  • 1张小伟,王延荣,张潇,裴伟.涡轮机械叶片的流固耦合数值计算方法[J].航空动力学报,2009,24(7):1622-1626. 被引量:44
  • 2谢亮,徐敏,张斌,安效民.基于径向基函数的高效网格变形算法研究[J].振动与冲击,2013,32(10):141-145. 被引量:13
  • 3徐敏,陈士橹.CFD/CSD耦合计算研究[J].应用力学学报,2004,21(2):33-36. 被引量:40
  • 4Carta F O. Coupled blade-disk-shroud flutter instabilities in turbojet engine rotors[J]. Journal of Engineering for Power, 1967,89(3) :419-426.
  • 5Bendiksen O O. Aeroelastic problems in turbomachines [R]. AIAA Paper 90-1157,1990.
  • 6Moffatt S, He L. Blade forced response prediction for industrial gas turbines: Part I Methodologies[R].ASME Paper GT 2003 38640,2003.
  • 7He L. An Euler solution for unsteady flows around oscillating blades[J]. Journal of Turbomachinery, 1990,112 (4) 714 722.
  • 8Hall K C, Lorence C B. Calculation of three-dimensional unsteady flows in turbomachinery using the linearized harmonic euler equations[R]. ASME Paper 92-GT-136,1992.
  • 9KielbR E. CFD for turbomachinery unsteady flows--An aeroelastic design perspective [R]. AIAA Paper 2001- 16317,2001.
  • 10Ekici K,Voytovych D M, Hall K C. Time-linearized Navier Stokes analysis of flutter in multistage turbomachines [R], AIAA 2005 836,2005.

共引文献11

同被引文献28

引证文献4

二级引证文献9

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部