1991
DOI: 10.2172/5177561
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Numerical simulation of VAWT stochastic aerodynamic loads produced by atmospheric turbauence: VAWT-SAL code

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Cited by 16 publications
(7 citation statements)
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“…At s ¼ 0.2, the entire torque is low and negative values can be seen at the low TSRs of 1.8 and 2.2. This negative torque of the low solidity H-Darrieus makes self-starting of the wind turbine difficult [14], thereby requiring considerable time to reach the operational TSR. Therefore, the low solidity H-Darrieus is not suitable as a self-starting wind turbine, but suitable as an induction-type wind turbine.…”
Section: Resultsmentioning
confidence: 99%
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“…At s ¼ 0.2, the entire torque is low and negative values can be seen at the low TSRs of 1.8 and 2.2. This negative torque of the low solidity H-Darrieus makes self-starting of the wind turbine difficult [14], thereby requiring considerable time to reach the operational TSR. Therefore, the low solidity H-Darrieus is not suitable as a self-starting wind turbine, but suitable as an induction-type wind turbine.…”
Section: Resultsmentioning
confidence: 99%
“…Homicz [14] used a numerical code called VAWT-SAL (VAWT Stochastic Aerodynamic Load), which used a DMST (double-multiple-stream tube)) method and numerically estimates the random loads created by atmospheric turbulence. Homicz found the output power to decrease slightly with increased turbulence intensity, while for TSRs near the maximum power coefficient, power increased as the turbulence level was raised.…”
Section: Introductionmentioning
confidence: 99%
“…This gives the surface two properties that are very useful. First it is a solid surface, partitioning the flow into regions, and secondly the surface relates (approximately) to the boundaries of stream tubes, when you realize that a stream tube can be any arbitrary shape [Hom91].…”
Section: Domain Expert Evaluationmentioning
confidence: 99%
“…In one sense, the price paid for structural simplicity is aerodynamic com-plexity: VAWT aerodynamics is inherently unsteady, and highly nonlinear. However, the relatively recent development of several methods capable of predicting steadystate performance has greatly in-creased our understanding of VAWT aerodynamics [2].…”
Section: Introductionmentioning
confidence: 99%