The shocklet was observed based on NPLS techniques in supersonic turbulent mix layer wind tunnel with convective Mach number 1.

 
  • 在對流馬赫數為1.;24的超聲速湍流混合層風(fēng)洞中;以NPLS實(shí)驗技術(shù)為基礎觀(guān)察到了小激波結構。
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