z-logo
open-access-imgOpen Access
Innovative tail configuration : numerical VS wind tunnel test data
Author(s) -
Sylvie Dequand,
Arnaud Geeraert,
G. D. Mortchelewicz
Publication year - 2019
Publication title -
hal (le centre pour la communication scientifique directe)
Language(s) - Uncategorized
Resource type - Conference proceedings
Subject(s) - aeroelasticity , airfoil , flutter , aerodynamics , wind tunnel , transonic , aerodynamic force , aerospace engineering , structural engineering , mechanics , angle of attack , flow (mathematics) , engineering , physics

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom