Rotational augmentation of horizontal axis wind turbine blade aerodynamic response

[1]  Maureen Hand,et al.  HAWT dynamic stall response asymmetries under yawed flow conditions , 2000 .

[2]  M Robinson,et al.  Unsteady aerodynamics of wind turbines , 1995 .

[3]  Göran Ronsten,et al.  Static pressure measurements on a rotating and a non-rotating 2.375 m wind turbine blade. Comparison with 2D calculations , 1992 .

[4]  Jonathan Whale,et al.  Correcting inflow measurements from hawts using a lifting-surface code , 1999 .

[5]  Mc Croskey Measurements of boundary layer transition, separation and streamline direction on rotating blades , 1971 .

[6]  J. F. Wellicome,et al.  Wind tunnel investigation of stall aerodynamics for a 1.0 m horizontal axis rotor , 1992 .

[7]  George Dettleff,et al.  Plume flow and plume impingement in space technology , 1991 .

[8]  W. H. H. Banks,et al.  DELAYING EFFECT OF ROTATION ON LAMINAR SEPARATION , 1963 .

[9]  M. Leroy Spearman,et al.  Wind-Tunnel Tests at Low Speed of Swept and Yawed Wings Having Various Plan Forms , 1951 .

[10]  Michael Robinson,et al.  Horizontal Axis Wind Turbine Aerodynamics: Three-Dimensional, Unsteady, and Separated Flow Influences , 1999 .

[11]  Michael Robinson,et al.  CONTRASTING BLADE FLOW FIELD ARCHETYPES IN THE HAWT OPERATING REGIME , 2001 .

[12]  M. C. Robinson,et al.  Evidence that aerodynamic effects, including dynamic stall, dictate HAWT structural loads and power generation in highly transient time frames , 1994 .

[13]  C. P. Butterfield,et al.  An overview of the Unsteady Aerodynamics Experiment phase 3 data acquisition system and instrumentation , 1995 .

[14]  David Simms,et al.  Unsteady aerodynamics associated with a horizontal-axis wind turbine , 1996 .

[15]  P. F. Yaggy,et al.  Laminar boundary layers on helicopter rotors in forward flight. , 1968 .