Heat flux reduction mechanism induced by a combinational opposing jet and cavity concept in supersonic flows

Authors:
  • WHWei Huang
    Wei Huang
  • YJYan-Ping Jiang
    Yan-Ping Jiang
  • LYLi Yan
    Li Yan
  • JLJun Liu
    Jun Liu

Abstract
No abstract available
Funding Information
  • Science Foundation of National University of Defense Technology (JC14-01-01)
  • National Natural Science Foundation of China (No.11502291)

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