首页> 外文会议>International Space Planes and Hypersonic Systems and Technologies Conference >Comparison between Probe Stagnation Point Heat Flux Measurements and Correlation Formulas in SCIROCCO Plasma Wind Tunnel Tests
【24h】

Comparison between Probe Stagnation Point Heat Flux Measurements and Correlation Formulas in SCIROCCO Plasma Wind Tunnel Tests

机译:探针停滞点热通量测量与探测探测点热通量测量和相关公式的比较

获取原文

摘要

A large part of the SCIROCCO Arc Heater Performance Map has been investigated. The heat flux measurements at the stagnation point of the facility Calibratio Probe have been used to find an experimental fit. Such a formula has been compared with the predictions of the De Filippis-Serpico equation and the well known Fay-Riddell formula. Finally the experimental fit has been also compared with the Sagner-Vèrant formula obtained at the ONERA F4 hypersonic plasma wind tunnel.
机译:已经调查了大部分Scirocco电弧加热器性能图。在设施校准探针的停滞点处的热通量测量已被用于寻找实验合适。已经将这种公式与De Filippis-Serpico方程的预测进行了比较,并且已知的用于众所周知的Fay riddell公式。最后,还与Onera F4超声等离子体风洞所获得的Sagner-Vèrant配方进行比较。

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