A reduced-order model for the investigation of the aeroelasticity of circulation-controlled wings

被引:1
作者
Krukow I. [1 ]
Dinkler D. [1 ]
机构
[1] TU Braunschweig, Institut fur Statik, Beethovenstr. 51, Braunschweig
关键词
Aeroelasticity; Circulation control; Modal reduction; Non-linear; Reduced-order model;
D O I
10.1007/s13272-013-0097-5
中图分类号
学科分类号
摘要
The application of active circulation control allows shortening of runways which can be significant in particular cases. The goal of the present paper is to study the influence of the circulation control on the aeroelastic behaviour of wings. For numerical analyses, a simplified computational model is presented, which allows for systematic parameter variations. The model is based on model reduction using modal analysis, so that an efficient performance of numerical studies is possible as well as the integration of the aeroelasticity into a flight dynamics model. © Deutsches Zentrum fu¨r Luft- und Raumfahrt e.V. 2014.
引用
收藏
页码:145 / 156
页数:11
相关论文
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