Author/Authors :
L. Djayapertapa، نويسنده , , C. B. Allen، نويسنده , , S. P. Fiddes، نويسنده ,
Abstract :
A computational method to perform transonic aeroelastic and aeroservoelastic calculations in the time
domain is presented, and used to predict stability (:utter) boundaries of 2-D wing sections. The aerodynamic
model is a cell-centred
Keywords :
transonic :ow , backlash , aeroelasticity , aeroservoelasticity , free-play , active :utter suppression
Journal title :
International Journal for Numerical Methods in Engineering
Journal title :
International Journal for Numerical Methods in Engineering