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两种高精度高效率静气弹数据传递函数
引用本文:贾欢,孙秦.两种高精度高效率静气弹数据传递函数[J].航空计算技术,2011,41(6):45-48.
作者姓名:贾欢  孙秦
作者单位:西北工业大学航空学院,陕西西安,710072
基金项目:中航工业产学研创新项目资助
摘    要:遵循静气弹问题中气动/结构网格之间的数据传递要求,引入了基于径向基函数的流固耦合界面数据传递方法,确定了紧支半径的选取原则,并编制相应的计算程序。以M6机翼为例,将不同径向基函数的插值精度及计算效率进行比较,结果表明体样条(Volume Spline)函数和C2函数具有良好的插值精度和计算效率。这两种流固耦合界面数据传递方法非常适用于工程应用。

关 键 词:流固耦合  径向基函数  数据传递  静气弹

Two Data Transfer Functions with High Accuracy and Efficiency for Aeroelasiticity Simulation
JIAN Huan,SUN Qin.Two Data Transfer Functions with High Accuracy and Efficiency for Aeroelasiticity Simulation[J].Aeronautical Computer Technique,2011,41(6):45-48.
Authors:JIAN Huan  SUN Qin
Institution:(School of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China)
Abstract:Following the requirements of data transfer between the fluid-structure girds in aeroelasticity,a method based on radial basis function is introduced.A principle about how to chose compact support radius and a coupling program is proposed.Taking M6 wing as a example,we compare different functions in accuracy and efficiency.It is turn out that volume spline function and compact radial function C2 show good performance in accuracy and efficiency.These two fluid-structure interaction functions are suitable for engineering application.
Keywords:fluid-structure interaction  radial basis function  data transfer  aeroelasticity
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