期刊文献+

垂尾抖振响应工程计算方法研究 被引量:2

Study on the Engineering Calculation Method for Vertical Tail Buffet Response
下载PDF
导出
摘要 分析了突风响应计算与抖振响应计算在计算原理上的差异,并提出一种修改NASTRAN突风响应计算流程作为进行抖振响应计算的方法。该方法可以采用刚性模型风洞试验测得的参考点脉动压力数据作为输入激励,翼面运动产生非定常气动力贡献则可以突风响应计算中偶极网格法计算模块计算。在NASTRAN软件的基础上,应用DMAP语言进行SOL 146求解器求解流程的修改,实现了抖振响应计算程序的二次开发,实现了突风载荷计算的屏蔽和抖振激励载荷的表征和输入处理。算例验算表明了算法的可行性。 The differences between gust response computation and buffet response computation are analyzed,and a calculation method for buffet response by modifying gust response computational procedure of the NASTRAN software is proposed.This method uses the power spectral density of the fluctuation pressure obtained from the wind-tunnel test of a rigid model as the external excitation,and the aerodynamic forces due to vertical fin motion can be calculated using a subsonic doublet-lattice lifting surface method which has been involved in the gust response calculating module of NASTRAN solver.Base on the NASTRAN software,we re-developed a buffet response calculation software,which used the DMAP language to modify the computational procedure of NASTRAN gust response,and to shield the gust load calculation,and to realize the directly input of buffet force.Then,a numerical example was performed to validate the feasibility of the proposed method.
出处 《科学技术与工程》 2011年第10期2261-2265,共5页 Science Technology and Engineering
关键词 垂尾抖振 突风响应 气动弹性 NASTRAN vetical tail buffeting gust response aeroelasticity NASTRAN
  • 相关文献

参考文献8

  • 1Lee B H K. Vertical tail buffeting of fighter aircraft, Progress in Aer- ospace Sciences , 2000;36:193-279.
  • 2Anderson W D , Patel S R , Black C L. Low speed wind tunnel buffet testing on the F/A-22. 45th A1AA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, California: Palm Springs, 2004.
  • 3Simpson D L, Landry N, Roussel J, et al. The Canadian and Aus- tralian F/A-18 international follow-on structural test project. In: Proceedings of the ICAS 2002 Congress, Toronto, Canada, 2002.
  • 4Zimmerman N H , Ferman M A. Prediction of tail buffet loads for de- sign application, Vol I and II. Rept, July 1987;No NADC-88043-60.
  • 5Levinski O. Vertical tail dynamic response in vortex breakdown flow, DSTO-RR-0256, DSTO Platforms Seienees Laboratory,2003.
  • 6Zirmnerman N H, Ferman M A, Yurkovich R N, et al. Prediction of tail buffet loads for design application. AIAA Paper, 1989; No 89-1378.
  • 7Lee B H K. Statistical analysis of wing/fin buffeting response , Pro- gress in Aerospace Sciences, 2002;38.
  • 8Pototzky A S, Moses R W. A tail buffet loads prediction method for aircraft at high angles of attack. Forum on Aeroelasticity and Structural Dynamics, 2005.

同被引文献10

引证文献2

二级引证文献6

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