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.
Document type :
Reports
Complete list of metadatas

Cited literature [15 references]  Display  Hide  Download

https://hal-lara.archives-ouvertes.fr/hal-02101920
Contributor : Colette Orange <>
Submitted on : Wednesday, April 17, 2019 - 9:09:47 AM
Last modification on : Friday, May 17, 2019 - 1:39:21 AM

File

RR1996-35.pdf
Files produced by the author(s)

Identifiers

  • HAL Id : hal-02101920, version 1

Collections

Citation

L. Giraudeau, Georges Perrot, S. Petit, Bernard Tourancheau. Simulation d'écoulement tridimensionnel autour d'une aile de parapente.. [Research Report] LIP RR-1996-35, Laboratoire de l'informatique du parallélisme. 1996, 2+29p. ⟨hal-02101920⟩

Share

Metrics

Record views

10

Files downloads

17