Volume 3, 2012Progress in Flight Physics
|Page(s)||107 - 118|
|Section||Chapter Two. Shock Interaction|
|Published online||29 January 2013|
Low and high enthalpy shock wave / boundary layer interactions around cylinder-flare models
Fundamental and Experimental Aerodynamics Department
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.
© Owned by the authors, published by EDP Sciences, 2012