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...on vertical heated walls (A)]] || André Latrobe || CEA / DRN / Department de Thermohydraulique | [[Natural and mixed convection boundary layers on vertical heated walls (B)]] || Mike Rab

*Mean and turbulent flow properties show the presence of a shock-induced separation b *With strong interactions and with sidewalls present the separated flow zones are highly three dimension

...fects of Shock Wave Induced Separation. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM) Vol 114, Springer.</div> <div id="4">'''Dupont P., Haddad C., Debiève J.F.''', 2006, Space and time organization in a shock induced separated boundary layer, J. Fluid Mec

...tGrey;"| Christopher Lea || style="background-color:LightGrey;"| UK Health and Safety Laboratory | style="background-color:LightGrey;"|[[Blade tip and tip clearance vortex flow]]<!--[[Image:Star_red.jpg]]-->|| style="backgroun

for both applications and basic research. In many aeronautical compressors, shock waves are formed and generally lead to separation. The

presence of low and high velocity streaks that populates canonical boundary increases and further downstream the turbulence slowly relaxes toward its

8° and of 9.5° at the nominal Mach number 2.25. They are both separated. frequency unsteadiness found in such conditions, and affecting the