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== Plasma Flow == === Underlying Flow Regime 231-09 ===

=== Underlying Flow Regime - ===

== Plasma Flow == === Underlying Flow Regime 231-09 ===

=== Underlying Flow Regime - ===

=== Underlying Flow Regime 123-432 ===

= Test Flow Challenge = === Underlying Flow Regime 51-792 ===

=== Underlying Flow Regime 123-432 ===

...contributors who intend to write Application Challenge or Underlying Flow Regime articles. == Underlying Flow Regimes ==

=== Underlying Flow Regime 51-792 ===

=== Underlying Flow Regime 7-01 ===

All Application Challenge (AC) and Underlying Flow Regime (UFR) articles in the Knowledge Base have been quality checked with the aid [http://qnetkb.cfms.org.uk/QR/D33_ufr_qr_template.doc Underlying Flow Regime Quality Review]

==='''UFR: Underlying Flow Regime'''===

==='''UFR: Underlying Flow Regime'''===

=='''UFR: Underlying Flow Regime'''==

==='''UFR: Underlying Flow Regime'''===

! UFR !! Underlying Flow Regime !! Contributor !! Organisation | [[Blade tip and tip clearance vortex flow]] [[Image:Star_red.jpg]]|| Michael Casey || Sulzer Innotec AG

! UFR !! Underlying Flow Regime !! Contributor !! Organisation | [[Blade tip and tip clearance vortex flow]]<!--[[Image:Star_red.jpg]]-->|| Michael Casey || Sulzer Innotec AG

...ocedures for filling out an Application Challenge (AC) and Underlying Flow Regime (UFR) article. Each template has specific headings and sub-headings with cl [[Media:Wiki-UFR-Template.doc | Underlying Flow Regime Article Template (MicroSoft Word)]]&nbsp;&nbsp;[[Media:Wiki-UFR-Template.pd

='''Test Flow Challenge'''= Underlying Flow Regime 51-792

[http://qnetkb.cfms.org.uk/QR/D33_ufr_qr_template.doc Underlying Flow Regime Quality Review]

=== UFR: Underlying Flow Regime ===

Underlying Flow Regime 231-09

Underlying Flow Regime 123-432

Underlying Flow Regime -

Underlying Flow Regime -

Underlying Flow Regime 231-09

Underlying Flow Regime 123-432

Underlying Flow Regime 3-30

Underlying Flow Regime 123-432

Underlying Flow Regime 51-792

Underlying Flow Regime 1-07

Underlying Flow Regime -

Underlying Flow Regime 51-792

Underlying Flow Regime 231-09

=Flow and heat transfer in a pin-fin array= ===Underlying Flow Regime 4-18===

=Flow in a 3D diffuser= ===Underlying Flow Regime 4-16===

=Hot pulsatile impinging jet in cold cross flow: PJICF= ===Underlying Flow Regime 4-15===

Underlying Flow Regime 51-792

= Test Flow Challenge = Underlying Flow Regime 51-792

=High Reynolds Number Flow around Airfoil in Deep Stall= ===Underlying Flow Regime 2-11===

=A fluid-structure interaction benchmark in turbulent flow (FSI-PfS-1a)= ===Underlying Flow Regime 2-13===

=Flow over curved backward-facing step= ===Underlying Flow Regime 3-31===

Underlying Flow Regime 231-09

Underlying Flow Regime -

=Turbulent flow past a smooth and rigid wall-mounted hemisphere= ===Underlying Flow Regime 3-33===

Underlying Flow Regime 123-432

=Turbulent Flow Past Two-Body Configurations= ===Underlying Flow Regime 2-12===

===Underlying Flow Regime 7-01===

* Suggestions for new Application Challenge or Underlying Flow Regime categories

Underlying Flow Regime -

Underlying Flow Regime 231-09

===Underlying Flow Regime 7-01===

===Underlying Flow Regime 2-14===

=Test Flow Challenge= Underlying Flow Regime 51-792

===Underlying Flow Regime 4-19===

! UFR !! Underlying Flow Regime !! Contributor || Organisation | [[Pipe flow - rotating]] || Paolo Orlandi, Stefano Leonardi || Universita di Roma 'La S

Underlying Flow Regime 123-432

===Underlying Flow Regime 4-17===

===Underlying Flow Regime 3-32===

===Underlying Flow Regime 7-01===

===Underlying Flow Regime 2-15===

! UFR !! Underlying Flow Regime !! Contributor !! Organisation | [[Flow behind a blunt trailing edge]] || Charles Hirsch || Vrije Universiteit Brus

=== Underlying Flow Regime 3-36 === ...on on a smooth curved surface. The physically and industrially significant flow phenomenon remains challenging to predict with state-of-the-art RANS turbul

=== Underlying Flow Regime 7-01 ===

=== Underlying Flow Regime 7-01 ===

=== Underlying Flow Regime 7-01 ===

Underlying Flow Regime -

===Underlying Flow Regime 7-01===

= 3D flow around blades = Underlying Flow Regime 2-07 <font size="-2" color="#888888">               © copyright ER

Underlying Flow Regime 231-09

= Curved passage flow = Underlying Flow Regime 4-05 <font size="-2" color="#888888">               © copyright ER

Underlying Flow Regime 123-432

= Curved passage flow = Underlying Flow Regime 4-05 <font size="-2" color="#888888">               © copyright ER

! UFR !! Underlying Flow Regime !! Contributor !! Organisation | [[Stagnation point flow]] || Beat Ribi || MAN Turbomaschinen AG Schweiz

All Application Challenge (AC) and Underlying Flow Regime (UFR) articles within the Knowledge Base have been quality checked with the

=Cylinder-wall junction flow= == Underlying Flow Regime 3-35 ==

= Flow around airfoils (and blades) A-airfoil (Ma=0.15,<br />Re/m=2x10⁶ Underlying Flow Regime 2-05 <font size="-2" color="#888888"> © copyright ERCOFTAC 2

=Cylinder-wall junction flow= == Underlying Flow Regime 3-35 ==

=== Underlying Flow Regime 2-10 === The flow past finite-height cylinders mounted on a wall is of considerable, practica

Underlying Flow Regime 4-13 <font size="-2" color="#888888">               © copyright ER ...mbustion chamber of reciprocating engine. It has given rise to interesting flow phenomena such as vortex breakdown, which are not yet fully understood.

= Flow and heat transfer in a pin-fin array = === Underlying Flow Regime 4-18 ===

= Flow around (airfoils and) blades (transonic) = Underlying Flow Regime 2-06 <font size="-2" color="#888888">               © copyright ER

=Flow over curved backward-facing step= ===Underlying Flow Regime 3-31===

= Cylinder-wall junction flow = == Underlying Flow Regime 3-35 ==

===Underlying Flow Regime 3-36=== # <div id="3">'''S. Zhang and S. Zhong''' Turbulent Flow Separation over a Two-Dimensional Ramp Using Synthetic Jets. '' AIAA Journa

= Flow in a curved rectangular duct - non rotating = Underlying Flow Regime 4-04 <font size="-2" color="#888888">               © copyright ER

=Flow and heat transfer in a pin-fin array= ===Underlying Flow Regime 4-18===

= Flow around airfoils (and blades) A-airfoil (Ma=0.15,<br />Re/m=2x10⁶ Underlying Flow Regime 2-05 <font size="-2" color="#888888"> © copyright ERCOFTAC 2

.... It follows from complicated geometry of flow passages, three-dimensional flow character with substantial effects of secondary flows, shock-wave/boundary- ...action with the turbulent boundary layer. The wakes in the supersonic exit regime are relatively thin.

= Turbulent Flow Past Two-Body Configurations = ===Underlying Flow Regime 2-12===

= Stagnation point flow = Underlying Flow Regime 3-12 <font size="-2" color="#888888">               © copyright ER

= Blade tip and tip clearance vortex flow  = Underlying Flow Regime 1-02 <font size="-2" color="#888888">               © copyright ER

= Blade tip and tip clearance vortex flow = Underlying Flow Regime 1-02 <font size="-2" color="#888888"> © copyright ERCOFTAC 2

=Fluid-structure interaction in turbulent flow past cylinder/plate configuration II (Second swiveling mode)= === Underlying Flow Regime 2-14 ===

===Underlying Flow Regime 3-32=== *Mean and turbulent flow properties show the presence of a shock-induced separation bubble.

=== Underlying Flow Regime 3-36 ===

= 2D flow over backward facing step  = Underlying Flow Regime 3-15 <font size="-2" color="#888888">               © copyright ER

Underlying Flow Regime 3-03 <font size="-2" color="#888888">               © copyright ER ...and consistently determine the onset and amount of separation under given flow conditions. For other technical devices, the separation prediction might no

=Fluid-structure interaction in turbulent flow past cylinder/plate configuration I (First swiveling mode)= === Underlying Flow Regime 2-13 ===

=== Underlying Flow Regime 3-36 === ...). Geometric variations of the test case were designed to achieve attached flow, incipient, moderate and strong separation. For the incipient configuration