Details

Autor(en) / Beteiligte

• Ali, Qazi Shahzad
• Kim, Man-Hoe

Titel

Design and performance analysis of an airborne wind turbine for high-altitude energy harvesting

Ist Teil von

• Energy (Oxford), 2021-09, Vol.230, p.120829, Article 120829

Ort / Verlag

Oxford: Elsevier Ltd

Erscheinungsjahr

2021

Quelle

Alma/SFX Local Collection

Beschreibungen/Notizen

• The airborne wind turbine (AWT) offers the opportunity to be installed in challenging heights. For this purpose, the present study focuses on the aerodynamic design of an airborne rotor lifted to high altitude from the viewpoint of airborne technology. The rotor blade is modeled by imposing the elevated wind dataset while the outer shape is comprised of multi-profiles of thick airfoils. Numerical approaches of the BEM and RANS-CFD are employed for insight into performance analysis. The extracted results of the CFD data agreed well with the empirical computations. The induced effect of the diffuser on the rotor is demonstrated through an auxiliary shell structure. A range of 3D simulations varying the airloads are conducted to investigate the on-design and off-design behavior of the rotor. The power coefficient (Cp), effective forces and mass amplification are computed and discussed in terms of performance indicators. The design analysis reveals the significance of the chosen design specification to an operational height of 400 m. The noticeable finding confirms that the optimal Cp of the resulting rotor always occurs at rated conditions and equally valid for both configurations. Additionally, a power gain of 21.3% is obtained from the rotor equipped with the diffuser geometry. •Aerodynamic design of the 3-bladed airborne rotor in bare and shell configurations.•Sensitivity analysis of the rotor at 400 m altitudes with the BEM-CFD comparison.•Empirical formulation of the rotor comprised of elevated wind climate conditions.•3D simulations of the full-scale energy system for a range of performance variables.•Power augmentation by 21.3% for the resulting rotor in the diffuser configuration.