Low and high enthalpy shock wave / boundary layer interactions around cylinder-flare models

The paper describes four test-cases around the same configuration type: a hollow cylinder flare model. The first three test-cases are relative to cold hypersonic flow and the fourth one to hot hypersonic flow: (i) a purely laminar low enthalpy interaction performed at Mach 9.92; (ii) a transitional low enthalpy interaction performed at Mach 5; (iii) a fully low enthalpy turbulent interaction performed at Mach 5; and (iν) a high enthalpy interaction performed at Mach 9.4