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首页> 外文期刊>Journal of Fluids and Structures >Gust response: Simulation of an aeroelastic experiment by a fluid-structure interaction method
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Gust response: Simulation of an aeroelastic experiment by a fluid-structure interaction method

机译:阵风响应:通过流固耦合方法模拟气动弹性实验

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In this paper fluid-structure interaction simulations regarding a gust generator experiment are presented, which has been conducted in 2010 in the Transonic Wind Tunnel in Gottingen (DNW-TWG), Germany. The main objective of the experiment was the investigation of the dynamic response problem of an elastic wing model concerning an encountering generic gust induced by a gust generator. Fluid-structure simulations, using a finite element structural model and a computational fluid dynamics model based on time-accurate, Reynolds-averaged Navier-Stokes equations, are compared to the experiment to validate the numerical methodology. Comparisons include steady and unsteady deflections of the elastic wing and pressure distributions. Finally, the results of simulated transfer functions of the gust generator to the elastic wing are presented in comparison to the test data.
机译:本文介绍了有关阵风发生器实验的流固耦合模拟,该模拟已于2010年在德国哥廷根的跨音速风洞(DNW-TWG)中进行。实验的主要目的是研究弹性机翼模型的动态响应问题,该模型涉及由阵风发生器引起的一般阵风。使用有限元结构模型和基于时间精确,雷诺平均Navier-Stokes方程的计算流体动力学模型对流体结构进行了仿真,以验证数值方法的正确性。比较包括弹性机翼的稳态和非稳态挠度以及压力分布。最后,与测试数据进行比较,给出了阵风发生器到弹性机翼的模拟传递函数的结果。

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