首页> 外文会议>ESA SP-563; European Symposium on Aerothermodynamics for Space Vehicles; 20041108-11; Cologne(DE) >EXPERIMENTAL INVESTIGATION OF THERMAL FLUID/STRUCTURE INTERACTION IN HIGH ENTHALPY FLOW
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EXPERIMENTAL INVESTIGATION OF THERMAL FLUID/STRUCTURE INTERACTION IN HIGH ENTHALPY FLOW

机译:高焓流热流体/结构相互作用的实验研究

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摘要

In DLR's arc-heated facility L3K a test campaign was performed on a generic flap model. The model was particularly designed to show influence of thermal fluid/structure interaction when exposed to a high enthalpy flow. Intrusive and non-intrusive measurement techniques were applied to measure the surface temperature distribution and temperature development inside the model. A special method was developed for a more comfortable analysis of infrared images. Comparison of the experimental data to the results of coupled numerical simulations of structure and flow field proved the necessity of considering thermal fluid/structure interactions for the flap configuration.
机译:在DLR的电弧加热设备L3K中,对通用襟翼模型进行了测试。该模型经过专门设计,可显示出在高焓流下热流体/结构相互作用的影响。应用侵入式和非侵入式测量技术来测量模型内部的表面温度分布和温度发展。开发了一种特殊的方法来更舒适地分析红外图像。将实验数据与结构和流场耦合数值模拟的结果进行比较,证明了考虑襟翼构型的热流体/结构相互作用的必要性。

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