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考虑机身干扰的机翼气动外形综合优化
引用本文:孙美建,詹浩,巩鹏潇.考虑机身干扰的机翼气动外形综合优化[J].西北工业大学学报,2011,29(3):329-334.
作者姓名:孙美建  詹浩  巩鹏潇
作者单位:西北工业大学航空学院,陕西西安,710072
基金项目:西北工业大学研究生创新实验中心
摘    要:由于受机身绕流的影响,后掠机翼翼根的流动非常复杂,翼根气动设计是后掠机翼气动设计的难点.本章发展了基于Kriging代理模型的双层粒子群优化算法,结合雷诺平均N-S方程流场求解器进行了考虑机身干扰的机翼气动外形综合优化研究,在保证机翼相对厚度和容积不减的前提下降低了气动阻力、低头力矩和翼根弯矩.而考虑非设计巡航状态的多...

关 键 词:粒子群优化算法  Kriging代理模型  机翼  机身干扰  数值模拟

A Better Aerodynamic Shape Optimization Method for Wing with Fuselage Interference Considered
Sun Meijian,Zhan Hao,Gong Pengxiao.A Better Aerodynamic Shape Optimization Method for Wing with Fuselage Interference Considered[J].Journal of Northwestern Polytechnical University,2011,29(3):329-334.
Authors:Sun Meijian  Zhan Hao  Gong Pengxiao
Affiliation:(College of Aeronautics,Northwestem Polytechnical University,Xi′an 710072,China)
Abstract:Aim.The introduction of the full paper reviews some papers in the open literature and then proposes our better optimization method,which is explained in sections 1 and 2.Section 1 presents the double-layer quantum-behaved particle swarm optimization(QPSO) algorithm that uses the Kriging surrogate model.Considering fuselage interference,section 2 optimzes the aerodynamic shape of a wing,using the Reynolds-averaged Navier-Stokes flow solver;its core consists of:(1) we use the Hicks-Henne analytical function m...
Keywords:wings  fuselages  optimization  algorithms  Navier-Stokes equations  simulation  quantum-behaved particle swarm optimization(QPSO) algorithm  Kriging surrogate model  fuselage interference  
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