Guide alphabétique, de la thermodynamique, amplification de chaleur, transfert de masse, et dynamique des fluides
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Stability failure of a half-wing model at 25 m/s and frequencies ~4.0 and ~9 Hz in the case without disturbance

This movie shows recording of a flutter phenomenon received on a dynamically similar model of aircraft half-wing in a clean stream of certified wind tunnel in Novosibirsk Aviation Technical College. The critical velocity of flexural–torsional flutter of cantilever as 25 m/s at a frequency of 4 Hz.

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 : 4836 Article ajouté : 13 June 2018 Dernière modification de l'article : 13 June 2018 © Copyright 2010-2021 Retour en haut de page