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基于边界涡量流的二维叶型优化建模与求解
引用本文:杨小娟,刘若阳,佘志坤.基于边界涡量流的二维叶型优化建模与求解[J].航空工程进展,2015,6(4):405-411.
作者姓名:杨小娟  刘若阳  佘志坤
作者单位:北京航空航天大学 数学与系统科学学院,北京航空航天大学,北京航空航天大学
基金项目:国家自然科学基金重大项目“基于流线场共轭映射的复杂曲面高精度数控加工新方法”
摘    要:针对二维叶片整体造型优化问题,提出一种基于边界涡量流的二维叶型优化模型,并对该模型进行求解。建立以含参数的Bezier曲线定义的二维叶型型线为边界、以边界涡量流正峰值的最小化为目标函数的优化模型,通过分析边界涡量流的生成机制,把叶型型线边界信息代入边界涡量流中,将边界涡量流用叶型型线参数和型线上的气动参数表示,进而获得新的目标函数表达式。该目标函数表达式可直接对叶型型线参数求导,仅使用简单的定步长梯度算法即可对优化模型求解。结果表明:优化后的叶型型线上的边界涡量流的正峰值显著降低。

关 键 词:    词:二维叶型  边界涡量流  Bezier曲线  梯度算法
收稿时间:2015/8/21 0:00:00
修稿时间:2015/10/2 0:00:00

The Optimization Model and Solution of Two-dimensional Compressor Blade Based on Boundary Vorticity Flux
Yang Xiaojuan,Liu ruoyang and shezhikun.The Optimization Model and Solution of Two-dimensional Compressor Blade Based on Boundary Vorticity Flux[J].Advances in Aeronautical Science and Engineering,2015,6(4):405-411.
Authors:Yang Xiaojuan  Liu ruoyang and shezhikun
Institution:School of Mathematics and System Sciences,Beihang University,Beihang University,Beihang University
Abstract:Concerning the optimization of two-dimensional compressor blade,a optimization model based on Boundary Vorticity Flux (BVF) was proposed and solved. Starting from a optimization model:the boundary is two-dimensional compressor blade defined by Bezier curve and the optimization target is the minimize of positive peak of Boundary Vorticity Flux (BVF), a new objective function is established through that the information of blade curve are brought into BVF by analyzing the reason of BVF production.The new objective function can get partial derivation of the parameters of blade curve,which make the simple gradient arithmetic being used to solve the built optimization model.The optimization experiment shows that the positive peak of Boundary Vorticity Flux is effectively decreasing in this process.
Keywords:two-dimensional compressor blade  Boundary Vorticity Flux  Bezier curve  gradient algorithm
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