首页> 外文会议>AIAA Aerospace Sciences Meeting;AIAA SciTech Forum >Large Eddy Simulation of the HIFiRE Direct Connect Rig Scramjet Combustor
【24h】

Large Eddy Simulation of the HIFiRE Direct Connect Rig Scramjet Combustor

机译:HIFiRE Direct Connect钻机Scramjet燃烧器的大涡模拟

获取原文

摘要

This paper presents recent results from a set of large eddy simulations (LES) related to the Hypersonic International Flight Research Experiment (HIFiRE). The focus of these calculations is on the ground based experiments performed in the HIFiRE Direct Connect Rig (HDCR). Through matching the geometry and conditions of the HDCR experiments, the goals of this work are to 1) investigate the turbulence and mixing characteristics of the high Reynolds flow with multi-species fuel injection, and 2) assess the resultant combustion regimes and finite-rate chemistry effects.
机译:本文介绍了与超声国际飞行研究实验(Hifire)相关的一组大型涡模拟(LES)的结果。这些计算的重点是在Hifire直接连接钻机(HDCR)中进行的基于地面的实验。通过匹配HDCR实验的几何和条件,这项工作的目标是1)研究高雷诺流量的湍流和混合特性,具有多种燃料喷射,2)评估所得燃烧制度和有限率化学效应。

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