|
|
|
|
|
Jafar S. Pilakkadan, Rafic M. Ajaj, Zawar Haider and Mohammadreza Amoozgar
This paper studies the aeroelastic behavior of a rectangular, cantilever wing equipped with the spanwise morphing trailing edge (SMTE) concept. The SMTE consists of multiple trailing edge flaps that allow controlling the spanwise camber distribution of a...
ver más
|
|
|
|
|
|
|
|
|
|
|
Chawki Abdessemed, Abdessalem Bouferrouk and Yufeng Yao
This work explores the aerodynamic and aeroacoustic responses of an airfoil fitted with a harmonically morphing Trailing Edge Flap (TEF). An unsteady parametrization method adapted for harmonic morphing is introduced, and then coupled with dynamic meshin...
ver más
|
|
|
|
|
|
|
|
|
|
|
Srinivas Vasista, Johannes Riemenschneider, Ralf Keimer, Hans Peter Monner, Felix Nolte and Peter Horst
A design for a new high lift system that features a morphing wing leading edge ?droop nose? has the potential to generate high lift coefficients whilst mitigating airframe noise emissions. This seamless, continuous, and stepless flexible droop nose poten...
ver más
|
|
|
|
|
|