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== Best Practice Advice == | == Best Practice Advice == | ||
The Knowledge Base contains: | The Knowledge Base contains: | ||
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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. | ||
{| border="1" | {| border="1" | ||
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| 2-07 || [[Confined double annular jet]] || [[Annular coaxial jets, flow and mixing|1-04]], [[Flow behind a blunt trailing edge|2-01]] | | 2-07 || [[Confined double annular jet]] || [[Annular coaxial jets, flow and mixing|1-04]], [[Flow behind a blunt trailing edge|2-01]] | ||
|- | |- | ||
! rowspan="7" |[[State-of-the-Art Review: Chemical | ! rowspan="7" |[[State-of-the-Art Review: Chemical, Process, Thermal and Nuclear Safety|AA3<br>State-of-the Art Review for Chemical, Process, Thermal Hydraulics and Nuclear Safety]] | ||
| 3-01 || [[Buoyancy-opposed wall jet]] || [[The plane wall jet|3-10]], [[Confined buoyant plume|4-09]] | | 3-01 || [[Buoyancy-opposed wall jet]] || [[The plane wall jet|3-10]], [[Confined buoyant plume|4-09]] | ||
|- | |- | ||
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| 3-11 || [[Downward flow in a heated annulus]] || [[Natural and mixed convection boundary layers on vertical heated walls (A)|3-06]], [[Natural and mixed convection boundary layers on vertical heated walls (B)|3-07]] | | 3-11 || [[Downward flow in a heated annulus]] || [[Natural and mixed convection boundary layers on vertical heated walls (A)|3-06]], [[Natural and mixed convection boundary layers on vertical heated walls (B)|3-07]] | ||
|- | |- | ||
! rowspan="5" |[[State-of-the Art Review: Civil Construction | ! rowspan="5" |[[State-of-the-Art Review: Civil Construction and HVAC|AA4<br>State-of-the Art Review for Civil Construction & HVAC]] | ||
| 4-01 || [[Wind environment around an airport terminal building]] || [[Flow over surface-mounted cube/rectangular obstacles |3-14]] | | 4-01 || [[Wind environment around an airport terminal building]] || [[Flow over surface-mounted cube/rectangular obstacles |3-14]] | ||
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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]] | ||
|- | |- | ||
! rowspan="1" |[[State-of-the Art Review: Environmental | ! rowspan="1" |[[State-of-the-Art Review: Environmental Flow|AA5<br>State-of-the Art Review for Environmental Flows]] | ||
|5-05 || [[Boundary layer flow and dispersion over isolated hills and valleys]] || [[Flow over an isolated hill (without dispersion)|3-13]] | |5-05 || [[Boundary layer flow and dispersion over isolated hills and valleys]] || [[Flow over an isolated hill (without dispersion)|3-13]] | ||
|- | |- | ||
! rowspan="9" |[[State-of-the Art Review: Turbomachinery Internal | ! rowspan="9" |[[State-of-the-Art Review: Turbomachinery Internal Flow|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= | | 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=2x10^6)|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= | | 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=2x10^6)|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]] | ||
|- | |- | ||
| 6-04 || [[Pump turbine]] || [[3D flow around blades|2-07]], [[Rotor/stator interaction|2-09]], [[2D Boundary layers with pressure gradients (A)|3-03]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Pipe flow - rotating|4-03]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]] | | 6-04 || [[Pump turbine]] || [[3D flow around blades|2-07]], [[Rotor/stator interaction|2-09]], [[2D Boundary layers with pressure gradients (A)|3-03]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Pipe flow - rotating|4-03]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]] | ||
|- | |- | ||
| 6-05 || [[Annular compressor cascade with tip clearance]] || [[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= | | 6-05 || [[Annular compressor cascade with tip clearance]] || [[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=2x10^6)|2-05]], [[Flow around (airfoils and) blades (transonic)|2-06]], [[2D Boundary layers with pressure gradients (A)|3-03]], [[Laminar-turbulent boundary layer transition|3-04]], [[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]], [[Bypass transition on a flat plate|3-19]], [[Flow in a curved rectangular duct - non rotating|4-0]], [[Curved passage flow|4-05]] | ||
|- | |- | ||
| 6-06 || [[Gas Turbine nozzle cascade]] || [[2D Boundary layers with pressure gradients (A)|3-03]], [[Laminar-turbulent boundary layer transition|3-04]], [[Shock/boundary-layer interaction (on airplanes)|3-05]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Bypass transition on a flat plate|3-19]] | | 6-06 || [[Gas Turbine nozzle cascade]] || [[2D Boundary layers with pressure gradients (A)|3-03]], [[Laminar-turbulent boundary layer transition|3-04]], [[Shock/boundary-layer interaction (on airplanes)|3-05]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Bypass transition on a flat plate|3-19]] | ||
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| 6-07 || [[Draft tube]] || [[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]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]], [[Swirling diffuser flow |4-06]] | | 6-07 || [[Draft tube]] || [[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]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Flow in a curved rectangular duct - non rotating|4-04]], [[Curved passage flow|4-05]], [[Swirling diffuser flow |4-06]] | ||
|- | |- | ||
| 6-08 || [[High speed centrifugal compressor]] || [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m= | | 6-08 || [[High speed centrifugal compressor]] || [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6)|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]] | ||
|- | |- | ||
| 6-10 || [[Axial compressor cascade]] || [[2D Boundary layers with pressure gradients (A)|3-03]], [[Laminar-turbulent boundary layer transition|3-04]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Bypass transition on a flat plate|3-19]] | | 6-10 || [[Axial compressor cascade]] || [[2D Boundary layers with pressure gradients (A)|3-03]], [[Laminar-turbulent boundary layer transition|3-04]], [[Stagnation point flow|3-12]], [[2D Boundary layers with pressure gradients (B)|3-18]], [[Bypass transition on a flat plate|3-19]] | ||
|- | |- | ||
| 6-12 || [[Steam turbine rotor cascade]] || [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m= | | 6-12 || [[Steam turbine rotor cascade]] || [[Flow around (airfoils and) blades (subsonic)|2-04]], [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6)|2-05]], [[Flow around (airfoils and) blades (transonic)|2-06]], [[Laminar-turbulent boundary layer transition|3-04]], [[Shock/boundary-layer interaction (on airplanes)|3-05]], [[Bypass transition on a flat plate|3-19]] | ||
|} | |} | ||
Latest revision as of 08:55, 4 June 2008
Best Practice Advice
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.