2020
DOI: 10.1016/j.jweia.2019.104024
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The effects of the aerodynamic interaction on the performance of two Flettner rotors

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Cited by 33 publications
(19 citation statements)
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“…Marco et al [11][12][13] assessed the impact of aspect ratio, spin ratio and end plate diameter on Flettner rotor performance; endplates installed on the Flettner rotor had a good effect. In reference [14], the relative position and velocity ratio of two Flettner rotors were tested and the conclusion was drawn that the velocity ratio and relative position were the decisive factors determining the influence of aerodynamic interaction on the performance of Flettner rotors. The flow structures with different Reynolds Numbers and different spin rates were discussed.…”
Section: Introductionmentioning
confidence: 99%
“…Marco et al [11][12][13] assessed the impact of aspect ratio, spin ratio and end plate diameter on Flettner rotor performance; endplates installed on the Flettner rotor had a good effect. In reference [14], the relative position and velocity ratio of two Flettner rotors were tested and the conclusion was drawn that the velocity ratio and relative position were the decisive factors determining the influence of aerodynamic interaction on the performance of Flettner rotors. The flow structures with different Reynolds Numbers and different spin rates were discussed.…”
Section: Introductionmentioning
confidence: 99%
“…Condition (3.4) 2 aims at representing a regular inflow, which is expected to slightly modify after bypassing the obstacle, but then tends to recompose at the outflow face, as in (3.4) 3 (see [6] for experimental evidence). In fact, in a wind tunnel, the inflow is generated by a turbine (see the left picture in Figure 3.2), which usually reproduces a Poiseuille flow, which is faster at the midpoint of the inflow face and vanishes on the edges of this face, as modeled by (3.4) 2 .…”
Section: An Extension Results and Two New Inflow-outflow Modelsmentioning
confidence: 99%
“…Recent experimental and numerical evidence [6,37,38] shows that, at a sufficiently large distance behind the obstacle, the perturbed flow concentrates its turbulent motion mostly in the wake of the body, see Figure 1.1 for a wind tunnel experiment and [6,13] for some experimental data. It is then clear that different boundary conditions should be imposed on the outlet, see [21,23,28].…”
Section: Introductionmentioning
confidence: 99%
“…The power consumed by the motor and the thrust produced from the Flettner rotor will regulate the amount of the main engine power that can be replaced. The produced thrust can be calculated as the summation of the lift and drag forces in the ship direction (Ballini et al 2017 ; Bentin et al 2016 ; Bordogna et al 2020 ; Bordogna et al 2019 ; De Marco et al 2016 ; Kray et al 2012 ; Mittal and Kumar 2003 ; Traut et al 2014 ).…”
Section: Flettner Rotors’ Principles and Fundamentalsmentioning
confidence: 99%
“…can be calculated as a function of the rotor circulation Ω . The circulation can be calculated using known lift coefficients ( C L ) using Kutta-Joukowsky formula or from model tests (Abbot and Von Doenhoff 1959 ; Bordogna et al 2020 ). The relation between V ind.…”
Section: Flettner Rotor Modelingmentioning
confidence: 99%