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Numerical Investigations of Wake and Shock Wave Effects on Film Cooling Performance in a Transonic T
  • 所属机构名称：中国科学技术大学
  • 会议名称：Proc. of ASME Turbo Expo 2013 Power for Land, Sea and Air, GT2013-94544
  • 时间：2013.6.6
  • 成果类型：会议
  • 相关项目：发散冷却在高超声速飞行器中应用的基础问题研究
作者： Huazhao Xu|Jianhua Wang|Ting Wang|
同会议论文项目
发散冷却在高超声速飞行器中应用的基础问题研究
期刊论文 17 会议论文 12
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Numerical Investigations of Wake and Shock Wave Effects on Film Cooling Performance in a Transonic T
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