首页 | 本学科首页   官方微博 | 高级检索  
     

学科间载荷参数空间插值传递方法
引用本文:李立州,王婧超,吕震宙,岳珠峰. 学科间载荷参数空间插值传递方法[J]. 航空动力学报, 2007, 22(7): 1050-1054
作者姓名:李立州  王婧超  吕震宙  岳珠峰
作者单位:西北工业大学,航空学院,西安,710072;西北工业大学,力学与土木建筑学院,西安,710072
摘    要:针对多学科优化分析中面面耦合学科网格间载荷传递的问题, 提出了在参数空间中的三次函数插值传递方法.该方法将三维空间的源学科载荷点投影到二维参数空间平面上, 用三次插值函数对目标点载荷进行计算.此方法解决了叶片表面弯曲对载荷传递精度的影响.某涡轮叶片温度传递的结果表明本文的方法具有很高的精度. 

关 键 词:航空、航天推进系统  多学科优化设计  载荷传递  参数空间
文章编号:1000-8055(2007)07-1050-05
收稿时间:2006-06-12
修稿时间:2006-06-12

A load interpolation transfer method among disciplines in parametric space
LI Li-zhou,WANG Jing-chao,L Zhen-zhou,YUE Zhu-feng. A load interpolation transfer method among disciplines in parametric space[J]. Journal of Aerospace Power, 2007, 22(7): 1050-1054
Authors:LI Li-zhou  WANG Jing-chao  L Zhen-zhou  YUE Zhu-feng
Affiliation:1.School of Aviation, Northwestern Polytechnincal University, Xi'an 710072, China2.School of Mechanics Civil Engineering and Architecture, Northwestern Polytechnincal University, Xi'an 710072, China
Abstract:The multidisciplinary analysis(MDA) and optimization(MDO) of turbine blades introduce the needs of load transfer between computation fluid dynamics(CFD) models and computation structural mechanics(CSM) models,as meshes are mostly different on the disciplinary coupling interfaces.The direct interpolation method is the first and easiest method considered for this purpose.But this method requires fine meshes to reduce the influence of geometric curvature on transfer precision,which in turn will block the whole MDO process.In this paper an interpolation method in parametric space was proposed to transfer the loads.The coupled nodes of the dissimilarly meshed,the disciplinary interfaces were mapped into a flat parametric space in the method.There,the loads were transferred.During calculating load of a target node parameterized,several source nodes were selected in a small area around the target point.The load distribution in the area was fitted by a cubic function.Then,the load of the target point was calculated by the function.For the load are transferred in the flat parametric space in the method,the influence of geometric curvature on the interpolation precision is minimized,and the transfer accuracy is good enough even for coarse interface meshes.
Keywords:aerospace propulsion system  multidisciplinary design optimization  load transfer  parametric space
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号