2001
DOI: 10.1016/s0141-0296(00)00109-7
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Optimization of a design code for wind-turbine rotor blades in fatigue

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Cited by 29 publications
(17 citation statements)
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“…Nevertheless, typical loading spectra have been defined such as the eight proposed in the WISPER (Wind SPEctrum Reference) sequence [10]. These spectra can be used for the evaluation of new designs by simulation and to define appropriate test procedures.…”
Section: Fatigue Loading Experiencementioning
confidence: 99%
“…Nevertheless, typical loading spectra have been defined such as the eight proposed in the WISPER (Wind SPEctrum Reference) sequence [10]. These spectra can be used for the evaluation of new designs by simulation and to define appropriate test procedures.…”
Section: Fatigue Loading Experiencementioning
confidence: 99%
“…by Ronold and Christensen. 6 Such a calibration would involve deriving partial factors for (a subset of) all stochastic parameters, and selecting a set of factors that brings the failure probability close to the target value for a wide variety of load situations and critical locations. Instead, we consider fatigue failure of four different components (listed in Table II); failure of a component occurs because loads acting on it cause a crack in a critical location to form and grow.…”
Section: Finding the Optimal Partial Factorsmentioning
confidence: 99%
“…An early study of fatigue reliability of a blade joint was carried out by Veers [17] who described the structural reliability process as four steps: formulation that defines the failure criteria; transformation that converts correlated/uncorrelated random variables into the normal u-space; approximation that approximates the complex limit-state function in the u-space; and computation that calculates the reliability index. For simplicity, previous blade fatigue analyses often treat wind turbine blades as typical beam-like structures [41,[67][68][69][70]. From simple beam theory, explicit equations can be applied to calculate the stress/strain of wind turbine blades as a function of wind loads.…”
Section: Rotor Bladesmentioning
confidence: 99%
“…Fatigue stress was described in terms of the root mean square of the instantaneous stress, which was assumed to be an exponential function of wind speed [72]. Ronold et al [41,67] calculated the stress range at the root as a ratio between the moment range and the section modulus, while the moment range was calculated as a function of 10-minute mean wind speed and other parameters. Cyclic fatigue loading for turbine blades is derived by using a time-varying stochastic wind applied on a rotating rotor and based on the traditional Miner's rule [73].…”
Section: Rotor Bladesmentioning
confidence: 99%