An insight into the separate flow and stall delay for HAWT

Renewable Energy

Volumn 36, Issue 1, 2011, Pages 69-76

  Yu, Guohua ^a   Shen, Xin ^a   Zhu, Xiaocheng ^a   Du, Zhaohui ^a  

^a SHANGHAI JIAO TONG UNIVERSITY   (China)

Author keywords

Du Selig model; Effective angle of attack; Stall delay; Wind turbine aerodynamics

Indexed keywords

2D AIRFOILS; AERODYNAMIC FORCE COEFFICIENTS; CFD COMPUTATION; COMPUTATIONAL RESULTS; DERIVED DATA; DU-SELIG MODEL; EFFECTIVE ANGLE OF ATTACK; FLOW CHARACTERISTIC; LIFTING SURFACES; MATLAB CODE; REYNOLDS-AVERAGED NAVIER STOKES SOLVERS; SPANWISE FLOW; STALL DELAY; STEADY STATE; SUCTION SURFACES; UNSTEADY AERODYNAMICS; WIND SPEED; WIND TUNNEL EXPERIMENT; WIND TURBINE AERODYNAMICS; WIND TURBINE ROTORS;

AIRFOILS; ANGLE OF ATTACK; EXPERIMENTS; GAS DYNAMICS; NASA; THREE DIMENSIONAL; TURBOMACHINE BLADES; WIND POWER; WIND TUNNELS; WIND TURBINES;

COMPUTATIONAL FLUID DYNAMICS;

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; FLOW MODELING; FLOW PATTERN; NAVIER-STOKES EQUATIONS; REYNOLDS NUMBER; STEADY-STATE EQUILIBRIUM; THREE-DIMENSIONAL FLOW; WIND TUNNEL; WIND TURBINE; WIND VELOCITY;

EID: 79751513069     PISSN: 09601481     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.renene.2010.05.021     Document Type: Article

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