Enhanced delayed DES of shock wave/boundary layer interaction in a planar transonic nozzle

著录项

• 来源
  《International Journal of Heat and Fluid Flow》 |2019年第6期|359-365|共7页
• 作者

  Della Posta G.; Martelli E.; Ciottoli P. P.; Stella F.; Bernardini M.;

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• 作者单位

  Sapienza Univ Rome, Dept Mech & Aerosp Engn, Via Eudossiana 18, I-00184 Rome, Italy;

  Univ Campania L Vanvitelli, Dept Engn, Via Roma 29, I-81031 Aversa, Italy;

  Sapienza Univ Rome, Dept Mech & Aerosp Engn, Via Eudossiana 18, I-00184 Rome, Italy;

  Sapienza Univ Rome, Dept Mech & Aerosp Engn, Via Eudossiana 18, I-00184 Rome, Italy;

  Sapienza Univ Rome, Dept Mech & Aerosp Engn, Via Eudossiana 18, I-00184 Rome, Italy;

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• 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  Detached eddy simulation; Shock wave/Boundary layer interaction; Overexpanded nozzle;

  机译：分离涡模拟;冲击波/边界层相互作用;喷嘴过度膨胀;