2020
DOI: 10.1016/j.enconman.2020.113308
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Performance evaluation of an integrated floating energy system based on coupled analysis

Abstract: An integrated floating energy system consisting of different types of energy devices is an ideal option for reducing the levelized cost of energy by enhancing the power production capacity. This study proposes a concept of an integrated energy system by combining two tidal turbines with a floating wind turbine. In order to investigate the power performance and dynamic responses of the hybrid concept, a novel coupled aero-hydro-servo-elastic tool is developed based on a commercial hydrodynamic analysis software… Show more

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Cited by 40 publications
(12 citation statements)
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“…The numerical analysis method in this paper is implemented based on FAST and AQWA [25][26][27][28]. It contains:…”
Section: Development Of the Coupling Frameworkmentioning
confidence: 99%
“…The numerical analysis method in this paper is implemented based on FAST and AQWA [25][26][27][28]. It contains:…”
Section: Development Of the Coupling Frameworkmentioning
confidence: 99%
“…For the timedomain model, fully coupled six-degree-of-freedom motions are considered for the three models. Particularly for the analysis of the single FOWT and FWWP, a fully coupled aero-hydro-servo-elastic model is established based on AQWA using the F2A method proposed by Yang et al (2020).…”
Section: Mathematical Backgroundmentioning
confidence: 99%
“…By using AQWA, the parameters of Cummins equation are obtained from the frequency-domain results, and other effects such as the mooring system and PTO system are modelled as additional loads added into Cummins equation. The F2A method proposed by Yang et al (2020) is used to establish a dynamic coupling link between AQWA modules and the aero-servo-elastic modules of the OpenFAST, resulting in a fully coupled aero-hydro-servo-elastic-mooring-PTO time-domain model. In the AeroDyn module of OpenFAST, the aerodynamic load on the blades is calculated based on the blade element momentum (BEM) theory, which is mainly composed of lift and drag forces.…”
Section: Time-domain Modelmentioning
confidence: 99%
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“…The tangential induction velocity is obtained using the BEMT. The lift and drag coefficients are called by looking up the aerodynamic performance tables of each blade sectional airfoil to calculate the aerodynamic loads on each blade using the equations will be then calculated through the following equations [29]:…”
Section: Description Of the Aero-servo-elastic Modeling In F2amentioning
confidence: 99%