Difference between revisions of "Advice"

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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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{| border="1"
 
{| border="1"
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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.


State of the Art Reviews AC Best Practice Advice for Application Challenges Best Practice Advice for Associated UFRs
AA1
State-of-the Art Review for External Aerodynamics
1-01 Aero-acoustic cavity 3-03, 3-18
1-02 RAE M2155 Wing 3-03, 3-05, 3-18
1-04 Channel flow with wall injection 4-07
1-05 Ahmed body
1-08 L1T2 3 element airfoil 3-01, 3-03, 3-04, 3-05, 3-18
AA2
State-of-the Art Review for Combustion
2-01 Bluff body burner for CH4-HE turbulent combustion 2-01
2-03 Gas burner controlled by variable density and/or counterflow
2-05 Airflow cyclic variations in IC engines 4-13
2-06 The confined TECFLAM swirling natural gas burner 4-02, 4-08
2-07 Confined double annular jet 1-04, 2-01
AA3
State-of-the Art Review for Chemical & Process, Thermal Hydraulics & Nuclear Safety
3-01 Buoyancy-opposed wall jet 3-10, 4-09
3-02 Induced flow in a T-junction 4-03
3-03 Cyclone separator 4-03, 4-06
3-05 Buoyant gas air-mixing 4-09
3-08 Spray evaporation in turbulent flow 3-11
3-10 Combining/dividing flow in Y junction 3-11, 4-03
3-11 Downward flow in a heated annulus 3-06, 3-07
AA4
State-of-the Art Review for Civil Construction & HVAC
4-01 Wind environment around an airport terminal building 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 3-10, 4-09, 4-11
4-04 Tunnel fire
4-06 Aerodynamic analysis of the great belt bridge 2-02
AA5
State-of-the Art Review for Environmental Flows
5-05 Boundary layer flow and dispersion over isolated hills and valleys 3-13
AA6
State-of-the Art Review for Turbomachinery Internal Flows
6-02 Low-speed centrifugal compressor 1-02, 2-04, 2-05, 2-06, 3-03, 3-08, 3-10, 3-12, 3-18, 4-04, 4-05
6-03 Annular compressor cascade without clearance 2-04, 2-05, 2-06, 3-03, 3-08, 3-12, 3-18, 4-04, 4-05
6-04 Pump turbine 2-07, 2-09, 3-03, 3-12, 3-18, 4-03, 4-04, 4-05
6-05 Annular compressor cascade with tip clearance 1-02, 2-04, 2-05, 2-06, 3-03, 3-04, 3-08, 3-10, 3-12, 3-18, 3-19, 4-0, 4-05
6-06 Gas Turbine nozzle cascade 3-03, 3-04, 3-05, 3-18, 3-19
6-07 Draft tube 3-03, 3-08, 3-18, 4-04, 4-05, 4-06
6-08 High speed centrifugal compressor 2-04, 2-05, 2-06, 3-03, 3-08, 3-10, 3-12, 3-18, 4-04, 4-05
6-10 Axial compressor cascade 3-03, 3-04, 3-12, 3-18, 3-19
6-12 Steam turbine rotor cascade 2-04, 2-05, 2-06, 3-04, 3-05, 3-19