Flapping wing structures have drawn increasing attention for harvesting energy from flowing
fluids. This work proposes the application of an adaptive Gurney flap to the trailing end of a …

针对旋翼动态失速导致的非定常载荷增加和失速颤振问题, 开展了基于后缘小翼的翼型动态失速
主动控制试验研究, 试验雷诺数Re= 7.0× 105, 减缩频率k= 0.097. 采用动态压力测试手段 …

Large-eddy simulations (LESs) of low-Reynolds-number flow (Re= 50,000) over a
NACA0018 airfoil are performed to investigate flow control at the stall angle of attack (15 …

The flow around a pitching NACA0015 airfoil with an oscillating trailing-edge flap is
experimentally investigated to characterize the influence of the flap kinematics on the …

The effects of a harmonically deflected trailing-edge flap, actuated at different start times and
amplitudes but with frequency different from the airfoil motion, on the aerodynamic loads of …

This work explores the aerodynamic and aeroacoustic responses of an airfoil fitted with a
harmonically morphing Trailing Edge Flap (TEF). An unsteady parametrization method …

MIRZAVAND and Eslami [1] have presented the thermal buckling analysis of simply
supported functionally graded material (FGM) cylindrical shells that are integrated with the …

This paper investigates the effect of the Dynamically Morphing Leading Edge (DMLE) on the
flow structure and the behavior of dynamic stall vortices around a pitching UAS-S45 airfoil …

Low Reynolds number (Re< 500,000) aerodynamics is an active research area as it has
applications in micro-air vehicles (MAVs) and small unmanned aerial vehicles (UAVs)[1, 2] …

This paper presents a method for optimizing blade designs in smart rotors; the objective is to
maximize power regardless of wind conditions. An extensive analysis of what is known as …