Shock-induced leading-edge separation in hypersonic flows

HIGHLIGHTS

• who: Enschede and colleagues from the ‡ Present address: Physics of Fluids, Faculty of Science and Technology, University of TwenteInstitute of Science, Bengaluru, India have published the research work: Shock-induced leading-edge separation in hypersonic flows, in the Journal: (JOURNAL)
• what: The authors investigate the phenomenon of shock-induced leading-edge separation in hypersonic flows, as shown in figure 3. Under the present experimental conditions, the STN code (Shock Tube Nozzle calculations for equilibrium air by Krek and amp; Jacobs 1993) estimates an insignificant change in the specific_heat ratio of the free-stream air (γ ≈ 1 . . .
  

   

  

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