Rotational augmentation of horizontal axis wind turbine blade aerodynamic response
- 1 April 2002
- journal article
- research article
- Published by Wiley in Wind Energy
- Vol. 5 (2-3), 133-150
- https://doi.org/10.1002/we.68
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Contrasting blade flow field archetypes in the HAWT operating regimePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2001
- Plans for Testing the NREL Unsteady Aerodynamics Experiment 10m Diameter HAWT in the NASA Ames Wind Tunnel: Minutes, Conclusions, and Revised Text Matrix from the 1st Science Panel MeetingPublished by Office of Scientific and Technical Information (OSTI) ,2000
- HAWT dynamic stall response asymmetries under yawed flow conditionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Correcting inflow measurements from HAWTs using a lifting-surface codePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Unsteady aerodynamics associated with a horizontal-axis wind turbineAIAA Journal, 1996
- Unsteady aerodynamics of wind turbinesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Wind tunnel investigation of stall aerodynamics for a 1.0 m horizontal axis rotorJournal of Wind Engineering and Industrial Aerodynamics, 1992
- Static pressure measurements on a rotating and a non-rotating 2.375 m wind turbine blade. Comparison with 2D calculationsJournal of Wind Engineering and Industrial Aerodynamics, 1992
- Laminar boundary layers on helicopter rotors in forward flight.AIAA Journal, 1968
- DELAYING EFFECT OF ROTATION ON LAMINAR SEPARATIONAIAA Journal, 1963