首页> 外文会议>New beginnings: challenges for aerospace innovation >SIMULATIONS ON TRANSPIRATION COOLING FOR SUPERSONIC FLOW
【24h】

SIMULATIONS ON TRANSPIRATION COOLING FOR SUPERSONIC FLOW

机译:超声速发汗冷却的模拟

获取原文
获取原文并翻译 | 示例

摘要

For the present study the ITLR supersonicrncombustion experimental facility was used torninvestigate the transpiration cooling efficiency ofrnC/C materials. The tested sample had a porosityrnof ε=16.1% and was exposed to supersonic (M=2.1)rnflow conditions at moderate total temperature levelsrnof the main flow at Tt,g=450 K. The surfacerntemperature of the C/C material was measured withrnthermocouples and infrared thermography.rnThese experimental data were used to validate userdefinedrnsubroutines with the commercial CFD-ACErncode for the computation of the transpirationrncooling mechanisms within porous materials. Thernmethod follows a strongly coupled approach andrnaccounts also for the mass and momentum transportrnin the porous medium. The discretization schemernwas adapted locally in order to account for therndiscontinuities occurring at the interface.
机译:对于本研究,ITLR超音速燃烧实验设备用于研究rnC / C材料的蒸腾冷却效率。测试样品的孔隙率为ε= 16.1%,并在中等的总温度水平下暴露于超音速(M = 2.1)流动条件下,主流温度为Tt,g = 450K。C / C材料的表面温度用热电偶和热电偶测量。这些实验数据用于通过商业CFD-ACErncode验证用户定义的子程序,以计算多孔材料内的蒸腾冷却机理。该方法遵循强耦合方法,并且还考虑了多孔介质中的质量和动量传输。离散化方案在本地进行了调整,以解决界面处出现的不连续性。

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