Semi-confined Flows: Difference between revisions

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!3-07  
!3-07  
| [[Natural and mixed convection boundary layers on vertical heated walls (B)]] || [[British Energy]]
| [[Natural and mixed convection boundary layers on vertical heated walls (B)]] || [[British Energy]]
|-
|- style="background-color:silver;"
!3-08  
!3-08  
| [[3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation]] || [[CIRA]]
| [[3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation]] || [[CIRA]]
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!3-10  
!3-10  
| [[The plane wall jet]] || [[Vattenfall Utveckling AB]]
| [[The plane wall jet]] || [[Vattenfall Utveckling AB]]
|-
|- style="background-color:silver;"
!3-11  
!3-11  
| [[Pipe expansion (with heat transfer)]] || [[Magnox Electric]]
| [[Pipe expansion (with heat transfer)]] || [[Magnox Electric]]
|-
|- style="background-color:silver;"
!3-12  
!3-12  
| [[Stagnation point flow]] || [[MAN Turbomaschinen AG Schweiz]]
| [[Stagnation point flow]] || [[MAN Turbomaschinen AG Schweiz]]
|-
|- style="background-color:silver;"
!3-13  
!3-13  
| [[Flow over an isolated hill (without dispersion)]] || [[EDF - R&D Division]]
| [[Flow over an isolated hill (without dispersion)]] || [[EDF - R&D Division]]
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!3-15  
!3-15  
| [[2D flow over backward facing step]] || [[CIMNE]]
| [[2D flow over backward facing step]] || [[CIMNE]]
|-
|- style="background-color:silver;"
!3-18  
!3-18  
| [[2D Boundary layers with pressure gradients (B)]] || [[Computational Dynamics Ltd]]
| [[2D Boundary layers with pressure gradients (B)]] || [[Computational Dynamics Ltd]]

Revision as of 11:29, 7 April 2009

UFR Underlying Flow Regime Contributor
3-01 Boundary layer interacting with wakes under adverse pressure gradient - NLR 7301 high lift configuration CFS Engineering SA
3-03 2D Boundary layers with pressure gradients (A) AEA Technology
3-04 Laminar-turbulent boundary layer transition Technical University of Czestochowa
3-05 Shock/boundary-layer interaction (on airplanes) Qinetiq
3-06 Natural and mixed convection boundary layers on vertical heated walls (A) CEA / DRN / Department de Thermohydraulique
3-07 Natural and mixed convection boundary layers on vertical heated walls (B) British Energy
3-08 3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation CIRA
3-09 Impinging jet Université de Poitiers
3-10 The plane wall jet Vattenfall Utveckling AB
3-11 Pipe expansion (with heat transfer) Magnox Electric
3-12 Stagnation point flow MAN Turbomaschinen AG Schweiz
3-13 Flow over an isolated hill (without dispersion) EDF - R&D Division
3-14 Flow over surface-mounted cube/rectangular obstacles University of Southampton
3-15 2D flow over backward facing step CIMNE
3-18 2D Boundary layers with pressure gradients (B) Computational Dynamics Ltd
3-19 Bypass transition on a flat plate Fachhochschule Niederrhein
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