Journal of Energy · 1978 · 455 citations · 4 references
EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsFluid DynamicsWind EngineeringAerodynamic DesignAerodynamic TestingExperimental AerodynamicsLow-speed AerodynamicsWind Turbine TechnologyWind-tunnel TestingAerodynamic Performance TestingReynolds NumberReynolds Number EffectsRotor AerodynamicsRotor Performance AnalysisTurbine AerodynamicsTurbine PerformanceWind Turbine Aerodynamics
Fifteen configurations of a Savonius rotor wind turbine were tested in the Vought Corporation Systems Division 4.9- x 6.1-m Low Speed Wind Tunnel to determine aerodynamic performance. The range of values of the varied parameters was as follows: number of buckets, 2 and 3; nominal freestream velocity, 7 and 14 m/s; Reynolds number per meter, 4.32 x 10/sup 5/ and 8.67 x 10/sup 5/; rotor height, 1 and 1.5 m; rotor diameter (nominal), 1 m; bucket overlap, 0.0 to 0.1 m. The measured test variables were torque, rotational speed, and tunnel conditions. It is concluded that increasing Reynolds number and/or aspect ratio improves performance. The recommended configuration consists of two sets of two-bucket rotors, rotated 90 deg apart, with each rotor having a dimensionless gap width of 0.1 to 0.15.
4
Describing Uncertainty in Single Sample Experiments
S. J. Kline · Mechanical Engineering · 1953 · 6.6K citations
Computing, Mathematics, Statistics +11
The S-rotor and its applications
S. J. Savonius · Mechanical Engineering · 1931 · 244 citations
Engineering, Electrical Engineering, Mechanical Engineering +8
Aerodynamic performance of wind turbines
Robert E. Wilson, P. B. S. Lissaman, S.N. Walker · STIN · 1976 · 176 citations