WIND TUNNEL FLUTTER TESTING ON A HIGHLY FLEXIBLE WING FOR AEROELASTIC VALIDATION IN THE TRANSONIC REGIME WITHIN THE HMAEI PROJECT
IFASD ; 18. ; 2019 ; Savannah, Ga.
2020
Aufsatz (Konferenz)
Englisch
Static Aeroelastic Effects on a Transonic Indicial Response Wing Flutter Calculation
Online Contents | 1998
|WING DESIGN FOR WIND TUNNEL FLUTTER TESTING
TIBKAT | 2020
|