Open Access
| Issue |
Volume 3, 2012
Progress in Flight Physics
|
|
|---|---|---|
| Page(s) | 107 - 118 | |
| Section | Chapter Two. Shock Interaction | |
| DOI | https://doi.org/10.1051/eucass/201203107 | |
| Published online | 29 January 2013 | |
Progress in Flight Physics 3 (2012) 107-118
Low and high enthalpy shock wave / boundary layer interactions around cylinder-flare models
Fundamental and Experimental Aerodynamics Department
ONERA, Meudon
92190,
France
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