Advice: Difference between revisions
Jump to navigation
Jump to search
No edit summary |
No edit summary |
||
| (7 intermediate revisions by the same user not shown) | |||
| Line 1: | Line 1: | ||
== Best Practice Advice == | == Best Practice Advice == | ||
The Knowledge Base contains: | The Knowledge Base contains: | ||
| Line 10: | Line 8: | ||
* 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" | ||
| Line 21: | Line 20: | ||
| 1-04 || [[Channel flow with wall injection]] || [[Developing channel flow with mass injection through wall|4-07]] | | 1-04 || [[Channel flow with wall injection]] || [[Developing channel flow with mass injection through wall|4-07]] | ||
|- | |- | ||
| 1-05 || [[Ahmed body]] | | 1-05 || [[Ahmed body]] || | ||
|- | |- | ||
| 1-08 || [[L1T2 3 element airfoil]] || [[Boundary layer interacting with wakes under adverse pressure gradient - NLR 7301 high lift configuration|3-01]], [[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]] | | 1-08 || [[L1T2 3 element airfoil]] || [[Boundary layer interacting with wakes under adverse pressure gradient - NLR 7301 high lift configuration|3-01]], [[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]] | ||
|- | |||
! rowspan="5" |[[State-of-the-Art Review: Combustion|AA2<br>State-of-the Art Review for Combustion]] | |||
| 2-01 || [[Bluff body burner for CH4-HE turbulent combustion]] || [[Flow behind a blunt trailing edge|2-01]] | |||
|- | |||
| 2-03 || [[Gas burner controlled by variable density and/or counterflow]] || | |||
|- | |||
| 2-05 || [[Airflow cyclic variations in IC engines]] || [[Compression of vortex in cavity|4-13]] | |||
|- | |||
| 2-06 || [[The confined TECFLAM swirling natural gas burner]] || [[Confined coaxial swirling jets|4-02]], [[Orifice/deflector flow|4-08]] | |||
|- | |||
| 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, 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]] | |||
|- | |||
| 3-02 || [[Induced flow in a T-junction]] || [[Pipe flow - rotating|4-03]] | |||
|- | |||
| 3-03 || [[Cyclone separator]] || [[Pipe flow - rotating|4-03]], [[Swirling diffuser flow |4-06]] | |||
|- | |||
| 3-05 || [[Buoyant gas air-mixing]] || [[Confined buoyant plume|4-09]] | |||
|- | |||
| 3-08 || [[Spray evaporation in turbulent flow]] || [[Pipe expansion (with heat transfer)|3-11]] | |||
|- | |||
| 3-10 || [[Combining/dividing flow in Y junction]] || [[Pipe expansion (with heat transfer)|3-11]], [[Pipe flow - rotating|4-03]] | |||
|- | |||
| 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 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]] | |||
|- | |||
| 4-02 || [[Flow and Sediment Transport in a Laboratory Model of a stretch of the Elbe River]] || | |||
|- | |||
| 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]] || | |||
|- | |||
| 4-06 || [[Aerodynamic analysis of the great belt bridge]] || [[Flow past cylinder |2-02]] | |||
|- | |||
! 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]] | |||
|- | |||
! 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=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=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]] | |||
|- | |||
| 6-05 || [[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]] | |||
|- | |||
| 6-07 || [[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=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]] | |||
|- | |||
| 6-12 || [[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.