首页> 外文期刊>Acta astronautica >Uncertainty and sensitivity study on blunt body's drag and heat reduction with combination of spike and opposing jet
【24h】

Uncertainty and sensitivity study on blunt body's drag and heat reduction with combination of spike and opposing jet

机译:尖峰和反向喷射相结合的钝体减阻降热的不确定度和敏感性研究

获取原文
获取原文并翻译 | 示例
           

摘要

Uncertainty and sensitivity study of three main parameters including length-to-diameter ratio, nozzle radius and total pressure ratio on the drag and heat reduction for the blunt body with spike and opposing jet is conducted. According to the simulation results obtained from the computational fluid dynamics, the relationship between input parameters and aerodynamic force/heat is established via the point-collocation non-intrusive polynomial chaos method. Uncertainties of pressure and heat flux caused by changes of input parameters are quantified. Sensitivity analysis is carried out to determine key parameters affecting pressure and heat flux changes. The results indicate that changes of peak pressure and peak heat flux are resulted from significant change in reattachment shock strength which varies with input parameters. Sensitivity analysis reveals that the length-to-diameter ratio has huge influence on the uncertainty in the recirculation zone, while the nozzle radius dominates the uncertainty in the reattachment zone. Moreover, it is found that the nozzle radius has an enormous effect on peak pressure and peak heat flux, and a significant negative correlation between them is identified.
机译:进行了长径比,喷嘴半径和总压力比这三个主要参数的不确定性和敏感性研究,研究了带有尖峰和反向射流的钝体的阻力和热量减少。根据从计算流体动力学获得的模拟结果,通过点配置非侵入式多项式混沌方法建立了输入参数与空气动力/热量之间的关系。量化由输入参数的变化引起的压力和热通量的不确定性。进行灵敏度分析以确定影响压力和热通量变化的关键参数。结果表明,峰值压力和峰值热通量的变化是由于重新附着冲击强度的显着变化引起的,该变化随输入参数而变化。敏感性分析表明,长径比对回流区的不确定性有很大的影响,而喷嘴半径主导着回流区的不确定性。此外,发现喷嘴半径对峰值压力和峰值热通量具有巨大影响,并且在它们之间发现了显着的负相关性。

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