Transition prediction for a two dimensional Navier-Stokes solver applied to wind-turbine airfoils-Reference-Cited by-同舟云学术

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Transition prediction for a two dimensional Navier-Stokes solver applied to wind-turbine airfoils

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:2000 ASME Wind Energy Symposium
language:
Short-container-title:

Author:

Brodeur Robert¹,van Dam C.¹

Affiliation:

1. California, Univ., Davis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-47

Reference26 articles.

1. 'Amal, D. "Boundary-LayerTransition:Prediction, ApplicationtoDragReduction,"SkinFrictionDrag Reduction,AGARD Report786, 1992,pp.5-l through 5-59.

2. Linear Stability Theory Applied to Boundary Layers

3. 4SchneiderJ.,andEwald,B. "Integrationof Stability MethodsintoNavier-StokesSolversfor computationof TransonicAirfoils," AIAA 94-1849CP,1994.

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2. Experimental Study of the Plunging Motion with Unsteady Wind Tunnel Wall Interference Effects;Experimental Techniques;2011-02-18

3. Wind turbine wake aerodynamics;Progress in Aerospace Sciences;2003-08

4. The aerodynamic design of multi-element high-lift systems for transport airplanes;Progress in Aerospace Sciences;2002-02

5. Bubble induced unsteadiness on wind turbine airfoils;2002 ASME Wind Energy Symposium;2002-01-14

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