Articles | Volume 11, issue 11
https://doi.org/10.5194/wes-11-4147-2026
https://doi.org/10.5194/wes-11-4147-2026
Research article
 | 
10 Nov 2026
Research article |  | 10 Nov 2026

Computational aerodynamics for leading-edge inflatable kite design

Jelle Agatho Wilhelm Poland, Kasper Raphaël G. Masure, Oriol Cayon, and Roland Schmehl

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Cited articles

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Barnes, J. P.: Semi-Empirical Vortex Step Method for the Lift and Induced Drag Loading of 2D or 3D Wings, in: Proceedings of the 1997 World Aviation Congress, Anaheim, CA, USA, https://doi.org/10.2514/6.1997-5559, 1997. a
Batchelor, G.: An Introduction to Fluid Dynamics, Cambridge University Press, https://doi.org/10.1017/CBO9780511800955, 1967. a, b
Belloc, H.: Wind Tunnel Investigation of a Rigid Paraglider Reference Wing, J. Aircraft, 52, 703–708, https://doi.org/10.2514/1.C032513, 2015. a, b
Bhagwat, M. J. and Leishman, J. G.: Generalized Viscous Vortex Model for Application to Free-Vortex Wake and Aeroacoustic Calculations, in: Proceedings of the 58th Annual Forum and Technology Display of the American Helicopter Society International, https://www.researchgate.net/publication/255470975_Generalized_viscous_vortex_model_for_application_to_free-vortex_wake_and_aeroacoustic_calculations (last access: 16 February 2026), 2002. a
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Short summary
Soft inflatable kites are promising tools for renewable applications, but their unusual shape makes them difficult to analyse with conventional aerodynamic methods. A fast, accurate computer model is presented based on detailed airflow simulations and wind tunnel measurements. Aerodynamic forces are predicted within about 10% of experimental values while requiring far less computing time. It also helps designers to balance efficiency and stability, enabling faster, more reliable kite development.
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