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===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.