Experimental Investigations of Simulated Ice Accretions at High Reynolds Numbers in the Onera F1 Wind Tunnel.

2009 ◽  
Author(s):  
Denis CassouDeSalle ◽  
Anne Gilliot ◽  
Claude Geiler ◽  
Jean-Claude Monnier ◽  
Andy Broeren ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Reynolds Numbers ◽  
Experimental Investigations ◽  
High Reynolds Numbers ◽  
Ice Accretions ◽  
High Reynolds

Wind-tunnel experiments and separation control of a NACA4412 with 25○sweep at high Reynolds numbers

2022 ◽  
Author(s):  
Pierre-Yves Passaggia ◽  
Guillermo Lopez Quesada ◽  
Stéphane Loyer ◽  
Lucien Baldas ◽  
Jean-Christophe Robinet ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Reynolds Numbers ◽  
Separation Control ◽  
Wind Tunnel Experiments ◽  
High Reynolds Numbers ◽  
High Reynolds

An Intermittent High-Reynolds-Number Wind Tunnel

1977 ◽  
Vol 28 (4) ◽  
pp. 259-264 ◽  
Author(s):  
J L Stollery ◽  
A V Murthy
Keyword(s):  
Reynolds Number ◽  
Wind Tunnel ◽  
High Reynolds Number ◽  
Reynolds Numbers ◽  
Simple Method ◽  
High Reynolds Numbers ◽  
Reservoir Conditions ◽  
High Reynolds ◽  
Cryogenic Wind Tunnel ◽  
Performance Estimates

SummaryThe paper suggests a simple method of generating intermittent reservoir conditions for an intermittent, cryogenic wind tunnel. Approximate performance estimates are given and it is recommended that further studies be made because this type of tunnel could be valuable in increasing the opportunities for research at high Reynolds numbers.

scholarly journals Wind Tunnel Tests of Wind Turbine Airfoils at High Reynolds Numbers

2014 ◽  
Vol 524 ◽  
pp. 012012 ◽  
Author(s):  
E Llorente ◽  
A Gorostidi ◽  
M Jacobs ◽  
W A Timmer ◽  
X Munduate ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Wind Turbine ◽  
Reynolds Numbers ◽  
Wind Tunnel Tests ◽  
High Reynolds Numbers ◽  
High Reynolds ◽  
Turbine Airfoils

scholarly journals Flow Structure behind a Wing at High Reynolds Numbers

2018 ◽  
Vol 180 ◽  
pp. 02111 ◽  
Author(s):  
Václav Uruba ◽  
Zdeněk Pátek ◽  
Pavel Procházka ◽  
Vladislav Skála ◽  
David Zacho ◽  
...  
Keyword(s):  
Wind Tunnel ◽  
Flow Structure ◽  
Reynolds Numbers ◽  
Streamwise Direction ◽  
Vortical Structures ◽  
High Reynolds Numbers ◽  
Piv Measurement ◽  
High Reynolds

The stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to study the vortical structures oriented in the streamwise direction, which take place both in suction and pressure sides of the wing. The Reynolds numbers during the experiments in the 3 m wind tunnel range from 0.5 million up to 1.5 million.

Sign in / Sign up

Export Citation Format

Share Document