Bleed Air Spoiler Optimisation for AWE Purposes
An aerodynamic optimisation of upper surface bleed air control to minimise reel-in power loss for soft-kite-based Airborne Wind Energy systems
G.J. Fimpel (TU Delft - Aerospace Engineering)
Alexander Van Zuijlen – Mentor (TU Delft - Aerodynamics)
Mac Gaunaa – Mentor (Technical University of Denmark (DTU))
S. Watson – Graduation committee member (TU Delft - Wind Energy)
Paul Thedens – Mentor (SkySails Power)
W. A. Timmer – Graduation committee member (TU Delft - Wind Energy)
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Abstract
A key challenge in the Airborne Wind Energy industry is the minimisation of the time and energy required for the transfer and return phases inherent to the power cycles of ground-generator-based kite power systems. This thesis contributes to solving this problem by exploring the use of bleed air spoilers during the return phase in terms of their potential to improve the average cycle performance. To this end, a mathematical model is first introduced to evaluate the individual phases of the characteristic power pumping cycles in a general sense. This model is further used to demonstrate that a given kite configuration with the capacity to selectively lower its glide slope and/or resultant aerodynamic loading could improve the net power output of the system by around 30%. A CFD-based simulation environment for investigations of the effects induced by bleed air spoilers is developed using Simcenter STAR-CCM+. To establish the reliability of the setup, a first study revolves around its validation with experimental data from independent wind tunnel tests on bleed air spoilers effects on ram-air parachutes. The second CFD study is based on a standard kite geometry employed by SkySails Power GmbH. Two parameter studies testing the influence of spoiler size and chordwise position are carried out to investigate how bleed air spoilers are best used to reach the desired aerodynamic effects. The results show that bleed-air spoilers should ideally be applied in the vicinity of the suction peak and that relatively small spoiler geometries can already entail a major effect on the resultant flow field. It is predicted that the evaluated configurations would improve the system's overall performance by 9 to 18.3%, mostly due to substantial reductions in the glide ratio.