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Flow disturbance and stability failure of a half-wing model caused by the vortex generator at 18 m/s and frequencies ~4.0 and ~9 Hz


Flow disturbance and stability failure of a half-wing model caused by the vortex generator at 18 m/s and frequencies ~4.0 and ~9 Hz

This movie shows the influence of vortices on the flutter critical speed.

Read more in Experimental and theoretical researches on influence of parametric excitation on the flutter critical speed of aircraft model of wing.

Nombre de vues : 2952 Article ajouté : 13 June 2018 Dernière modification de l'article : 13 June 2018 © Copyright 2010-2020 Retour en haut de page