Investigation of aerodynamic interaction between the balloon and the ducted wind turbine in airborne configuration

Q2 Engineering Energy Harvesting and Systems Pub Date : 2022-01-01 DOI:10.1515/ehs-2021-0067
N. P. Noronha, Krishna Munishamaih
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Abstract

Abstract An aerodynamic analysis is presented in the current work, which estimates the separation distance between the balloon and the turbine in an airborne wind energy system (AWES). The stability of the structure of AWES depends on the aerodynamic interaction between the turbine and the balloon. A minimum gap must be maintained between the balloon and the wind turbine to reduce the interaction between the balloon and the turbine assembly. Three cases of AWES have been studied with a separation gap of 5 m, 10 m, and 16 m to estimate the minimum distance of separation between the balloon and the turbine. The aerodynamic interaction details suggest that a minimum distance of 13 m needs to be maintained between the turbine and the balloon to avoid the interaction between the balloon and turbine. Steady-state simulations of the rotor are run for various wind conditions to evaluate the efficiency of the duct-mounted configuration. The ducted turbine configuration saw a 7.4% increase in torque than the inducted turbine for a wind speed of 5 m s−1. A torque increase of 17.85% was observed when the separation distance was increased to 16 m from earlier 10 m.
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气动气球与风管式风力机的气动相互作用研究
摘要针对机载风能系统(awe)中气球与涡轮之间的分离距离进行了气动分析。awe结构的稳定性取决于涡轮和气球之间的气动相互作用。气球和风力涡轮机之间必须保持最小的间隙,以减少气球和涡轮机组件之间的相互作用。为了估算汽球与涡轮之间的最小距离,我们研究了三种分离间隙分别为5 m、10 m和16 m的情况。气动相互作用细节表明,涡轮与气球之间需要保持最小13 m的距离,以避免气球与涡轮之间的相互作用。在各种风力条件下对转子进行了稳态模拟,以评估管道安装结构的效率。当风速为5米/秒−1时,导管式涡轮机的扭矩比诱导式涡轮机增加了7.4%。当分离距离由10 m增加到16 m时,转矩增加了17.85%。
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来源期刊
Energy Harvesting and Systems
Energy Harvesting and Systems Energy-Energy Engineering and Power Technology
CiteScore
2.00
自引率
0.00%
发文量
31
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