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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.

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