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Simulation d'écoulement tridimensionnel autour d'une aile de parapente.
Abstract : This report presents our work for the design, model and implementation of a 3D air flow simulation software using the singularity method. The aim was the computation of the performance parameters of a wing at different speeds (between 10-60 km/h) with perfect uncompressible fluid and permanent flow hypothesis in order to help out with the design of paragliders. Sections 1 and 2 presents the model, design and the implementation and the results we obtained are in section 3.
Cited literature [15 references]
https://hal-lara.archives-ouvertes.fr/hal-02101920
Contributor : Colette Orange <>
Submitted on : Wednesday, April 17, 2019 - 9:09:47 AM
Last modification on : Wednesday, November 20, 2019 - 2:50:26 AM
Contributor : Colette Orange <>
Submitted on : Wednesday, April 17, 2019 - 9:09:47 AM
Last modification on : Wednesday, November 20, 2019 - 2:50:26 AM
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RR1996-35.pdf
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