Study of asymmetric hovering in flapping flight
Study of the unsteady aerodynamics of flapping airfoils has received a major boost in the
recent past for its application in the field of MAV design. The present study investigates the …
recent past for its application in the field of MAV design. The present study investigates the …
Secondary resonances in aeroelastic response of oscillating airfoil under dynamic stall
To clarify the mechanism of the complex aeroelastic responses of flexible blades of
helicopter rotors under dynamic stall, experiments on a 2D aeroelastic system are …
helicopter rotors under dynamic stall, experiments on a 2D aeroelastic system are …
Aerodynamic stiffness effect and sub-harmonic synchronization of aeroelastic system in the presence of dynamic stall
Z Qiu, F Wang - Journal of Fluids and Structures, 2021 - Elsevier
A computational study of forced aeroelastic system of an airfoil is performed under various
free-stream velocities. The results show that, as the free-stream velocity increases, the …
free-stream velocities. The results show that, as the free-stream velocity increases, the …
On aeroelastic response of an airfoil under dynamic stall using time delay neural network
Z Qiu, F Wang - Aerospace Systems, 2018 - Springer
To clarify the mechanism of the complex aeroelastic responses of flexible blades of
helicopter rotors under dynamic stall, an aeroelastic system of a 2D airfoil forced to oscillate …
helicopter rotors under dynamic stall, an aeroelastic system of a 2D airfoil forced to oscillate …
[PDF][PDF] 周期激励下NACA 0012 翼型单自由度失速颤振研究
阮胤， 邱展， 王福新 - 浙江大学学报(工学版), 2017 - researchgate.net
为了深入理解以周期变距为激励的失速颤振特性, 通过弹性机构输入周期变化角度,
进而控制NACA 0012 翼型攻角变化的实验装置, 探究弹性约束下翼型攻角的变化规律以及有/无 …
进而控制NACA 0012 翼型攻角变化的实验装置, 探究弹性约束下翼型攻角的变化规律以及有/无 …