NUMERICAL AERODYNAMIC OPTIMISATION OF 3D HIGH-LIFT CONFIGURATIONS

机译：3D高升降构型的数值气动优化

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The paper presents the numericalrnoptimisation activity carried out at DLR for therndesign of wing-body aircrafts in high-liftrnconfiguration. The purpose of the study is tornassess the high-fidelity methods and toolsrnneeded to optimise the flap and slat settings ofrn3D configurations in a limited turn-around time.rnThe selected key technologies are successfullyrnapplied for the optimisations of 2 different highliftrnconfigurations.

机译：本文介绍了在DLR进行的针对高升程配置的机翼飞机设计的数值优化活动。本研究的目的是评估在有限的周转时间内优化3D配置的襟翼和板条设置所需要的高保真度方法和工具。成功地将所选的关键技术应用于2种不同的高提升配置的优化。

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来源
《New beginnings: challenges for aerospace innovation》|2009年|p.1-11|共11页
会议地点 Manchester(GB)
作者
J. Brezillon; R.P. Dwight; J. Wild;
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作者单位

German Aerospace Center Institute of Aerodynamics and Flow Technology, Braunschweig, Germany;

German Aerospace Center Institute of Aerodynamics and Flow Technology, Braunschweig, Germany;

German Aerospace Center Institute of Aerodynamics and Flow Technology, Braunschweig, Germany;

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会议组织
原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
high-lift, optimisation, evolutionary strategy, adjoint approach, mesh strategy;

机译：高举，优化，进化策略，伴随方法，网格策略;

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专利

1. Applications of a discrete viscous adjoint method for aerodynamic shape optimisation of 3D configurations [J] . Joeel Brezillon, Richard P. Dwight CEAS Aeronautical Journal . 2012,第1期

机译：离散粘性伴随方法在3D外形气动形状优化中的应用
2. Model order reduction for steady aerodynamics of high-lift configurations [J] . Alexander Vendl, Heike Fassbender, Stefan Goertz, CEAS Aeronautical Journal . 2014,第4期

机译：减少模型顺序以实现高升程配置的稳定空气动力学
3. Numerically analyzing more efficiently high-lift aerodynamics of wing/body model with omni-tree Cartesian grids [J] . Weimin Sang, Jiangang Yu Aerospace science and technology . 2011,第5期

机译：用全树直角坐标网格更高效地数值分析机翼/机体模型的高空空气动力学
4. NUMERICAL AERODYNAMIC OPTIMISATION OF 3D HIGH-LIFT CONFIGURATIONS [C] . J. Brezillon, R.P. Dwight, J. Wild CEAS European air and space conference . 2009

机译：3D高升力配置的数值空气动力学优化
5. étude numérique de la dispersion des émissions de moteur dans le sillage tourbillonnaire d’un avion en configuration hypersustentée =Numerical Study of the Dispersion of Engine Emissions in the Swirling Wake of an Airplane in High-Lift Configuration [D] . Revelant, Maxime . 2019

机译：旋流膜中的数字发动机排放分散研究在高升力配置中发动机排放中发动机排放分散的数值研究
6. Configurations 3dn 4p + 3dn−1 4s4p in Sc II Ti II and V II [O] . C. Roth 1969

机译：Sc IITi II和V II中的配置3dn 4p + 3dn-1 4s4p
7. Applications of a discrete viscous adjoint method for aerodynamic shape optimisation of 3D configurations [O] . Brezillon, J., Dwight, R.P. 2012

机译：离散粘性伴随方法在3D外形气动形状优化中的应用
8. Unstructured Grid Generation for Complex 3D High-Lift Configurations [R] . Pirzadeh, Shahyar Z. 1999

机译：用于复杂3D高升力配置的非结构化网格生成

NUMERICAL AERODYNAMIC OPTIMISATION OF 3D HIGH-LIFT CONFIGURATIONS

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