Search results

= 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 ===

=Mixing ventilation flow in an enclosure driven by a transitional wall jet= === Underlying Flow Regime 4-20 ===