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* A State-of-the-Art Review on each Thematic Area, written by a leading expert in the field. | * A State-of-the-Art Review on each Thematic Area, written by a leading expert in the field. | ||
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| 4-03 || [[Air flows in an open plan air conditioned office]] || [[The plane wall jet |3-10]], [[Confined buoyant plume|4-09]], [[Simple room flow|4-11]] | | 4-03 || [[Air flows in an open plan air conditioned office]] || [[The plane wall jet |3-10]], [[Confined buoyant plume|4-09]], [[Simple room flow|4-11]] | ||
|- | |- | ||
| 4-04 || [[Tunnel fire]] || | | 4-04 || [[Tunnel fire]] || | ||
|- | |- | ||
| 4-06 || [[Aerodynamic analysis of the great belt bridge]] || [[Flow past cylinder |2-02]] | | 4-06 || [[Aerodynamic analysis of the great belt bridge]] || [[Flow past cylinder |2-02]] | ||
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! rowspan="9" |[[State-of-the Art Review: Turbomachinery Internal Flows|AA6<br>State-of-the Art Review for Turbomachinery Internal Flows]] | ! rowspan="9" |[[State-of-the Art Review: Turbomachinery Internal Flows|AA6<br>State-of-the Art Review for Turbomachinery Internal Flows]] | ||
|6-02 || [[Low-speed centrifugal compressor]] || [[Blade tip and tip clearance vortex flow |1-02]], [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x106)|2-05]], [[Flow around (airfoils and) blades (transonic)|2-06]], [[2D Boundary layers with pressure gradients (A)|3-03]], [[3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation|3-08]], [[The plane wall jet |3-10]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]] | | 6-02 || [[Low-speed centrifugal compressor]] || [[Blade tip and tip clearance vortex flow |1-02]], [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x106)|2-05]], [[Flow around (airfoils and) blades (transonic)|2-06]], [[2D Boundary layers with pressure gradients (A)|3-03]], [[3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation|3-08]], [[The plane wall jet |3-10]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]] | ||
|- | |- | ||
| 6-03 || [[Annular compressor cascade without clearance]] || [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x106)|2-05]], [[Flow around (airfoils and) blades (transonic)|2-06]], [[2D Boundary layers with pressure gradients (A)|3-03]], [[3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation|3-08]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]] | | 6-03 || [[Annular compressor cascade without clearance]] || [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x106)|2-05]], [[Flow around (airfoils and) blades (transonic)|2-06]], [[2D Boundary layers with pressure gradients (A)|3-03]], [[3D boundary layers under various pressure gradients, including severe adverse pressure gradient causing separation|3-08]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]] |
Revision as of 08:45, 4 June 2008
Best Practice Advice
[Note that this page was copied verbatim from the HTML used in the original QNET web site. It needs further work...]
The Knowledge Base contains:
- Best Practice Advice for each of the Underlying Flow Regimes that distils the experience of the European community of specialists into guidelines for ensuring quality of CFD simulations;
- Best Practice Advice for each of the Application Challenges based on existing knowledge, giving guidance to users attempting similar calculations to enable them to perform quality calculations and to interpret and deploy results with greater trust.
- A State-of-the-Art Review on each Thematic Area, written by a leading expert in the field.