2016
DOI: 10.1016/j.enconman.2016.06.004
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Multidisciplinary design optimization of large wind turbines—Technical, economic, and design challenges

Abstract: a b s t r a c tWind energy has experienced a continuous cost reduction in the last decades. A popular cost reduction technique is to increase the rated power of the wind turbine by making it larger. However, it is not clear whether further upscaling of the existing wind turbines beyond the 5-7 MW range is technically feasible and economically attractive. To address this question, this study uses 5, 10, and 20 MW wind turbines that are developed using multidisciplinary design optimization as upscaling data poin… Show more

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Cited by 70 publications
(32 citation statements)
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“…The first allows to maximize the AEP of the rotor, while the second minimizes the loads produced by the blades. Another formulation at system-level has been presented by Ashuri et al [21,22]. Here, a preliminary round of design can be made by optimizing blade length, tower height, and the rotor speed for minimum COE.…”
Section: State Of the Art In The Multidisciplinary Design Of Wind Turmentioning
confidence: 99%
“…The first allows to maximize the AEP of the rotor, while the second minimizes the loads produced by the blades. Another formulation at system-level has been presented by Ashuri et al [21,22]. Here, a preliminary round of design can be made by optimizing blade length, tower height, and the rotor speed for minimum COE.…”
Section: State Of the Art In The Multidisciplinary Design Of Wind Turmentioning
confidence: 99%
“…This option also increases the metric M2 by reducing the material factors f t of the components (j = 1,2, … n), which are part of the equivalent mass of the turbine -see also equation (13). This option also increases the metric M2 by reducing the material factors f t of the components (j = 1,2, … n), which are part of the equivalent mass of the turbine -see also equation (13).…”
Section: New Materialsmentioning
confidence: 99%
“…Conversely, the first edge natural frequencies decrease faster and faster when division locations are from 14 m to the blade tip. Figure 10b indicates that the second natural edge frequencies increase when the division location is within 6 m and between 24 and 30 m, and the increments of natural frequencies keep pace According to the scheme proposed in Section 2.3, we assumed that the stiffness of the SB-38 sectional blade increases with α of 4,6,8,9.62, and 12 as much as the original blade at the division location. At α = 9.62 is a specific characteristic for the CTC-38 blade, and the other values of 4, 6, 8, and 12 were also considered to study the impacts on natural frequencies.…”
Section: Natural Frequencies Variation Of Sectional Bladesmentioning
confidence: 99%
“…For T-bolted joints, , would be larger than that of the embedded sleeve connection. According to the scheme proposed in Section 2.3, we assumed that the stiffness of the SB-38 sectional blade increases with α of 4,6,8,9.62, and 12 as much as the original blade at the division location. At α = 9.62 is a specific characteristic for the CTC-38 blade, and the other values of 4, 6, 8, and 12 were also considered to study the impacts on natural frequencies.…”
Section: Natural Frequencies Variation Of Sectional Bladesmentioning
confidence: 99%
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