首页> 外文会议>European Symposium on Aerothermodynamics for Space Vehicles >EXPERIMENTAL INVESTIGATION OF THERMAL FLUID/STRUCTURE INTERACTION IN HIGH ENTHALPY FLOW
【24h】

EXPERIMENTAL INVESTIGATION OF THERMAL FLUID/STRUCTURE INTERACTION IN HIGH ENTHALPY FLOW

机译:高焓流动热流体/结构相互作用的实验研究

获取原文

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的弧度加热设施L3K上,在通用襟翼模型上进行测试活动。该模型特别设计用于在暴露于高焓流时显示热流体/结构相互作用的影响。应用侵扰性和非侵入式测量技术来测量模型内的表面温度分布和温度显影。开发了一种特殊方法,用于对红外图像进行更舒适的分析。实验数据对结构和流场耦合数值模拟结果的比较证明了考虑翼片配置的热流体/结构相互作用的必要性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号