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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 Rab4 KB (499 words) - 16:00, 17 February 2023
- *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 dimension3 KB (443 words) - 13:46, 12 February 2017
- ...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 Mec4 KB (522 words) - 13:46, 12 February 2017
- ...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="backgroun18 KB (1,983 words) - 15:58, 17 February 2023
- for both applications and basic research. In many aeronautical compressors, shock waves are formed and generally lead to separation. The10 KB (1,497 words) - 13:45, 12 February 2017
- presence of low and high velocity streaks that populates canonical boundary increases and further downstream the turbulence slowly relaxes toward its13 KB (1,855 words) - 13:45, 12 February 2017
- 8° and of 9.5° at the nominal Mach number 2.25. They are both separated. frequency unsteadiness found in such conditions, and affecting the24 KB (3,638 words) - 13:45, 12 February 2017