[en] The aeroelastic phenomena taking place on the Hyperloop structure are investigated on the basis of static aerodynamic and aeroelastic scaled models tested in wind tunnel. The post-critical regime is reached through the adjunction of roughness on the surface of the cylinders. The aeroelastic responses are analysed and the corresponding critical galloping and VIV wind speeds are compared to aeroelastic measurement data.
Research center :
Wind Tunnel Laboratory (University of Liège)
Disciplines :
Civil engineering Mechanical engineering
Author, co-author :
Andrianne, Thomas ; Université de Liège - ULiège > Aérospatiale et Mécanique (A&M)
