Within the transonic regime, the aeroelastic problems exhibit many unique characteristics
compared with subsonic and supersonic cases. Although a lot of research has been carried …

This paper explores the dynamical response of a two-degree-of-freedom flat plate
undergoing classical coupled-mode flutter in a wind tunnel. Tests are performed at low …

We conduct a computational study of flow-induced pitch oscillations of a rigid airfoil at a
chord-based Reynolds number of 1000. A sharp-interface immersed boundary method is …

This paper focuses on the effect of the phase offset of Leading-Edge (LE) morphing on the
aerodynamic characteristics of a pitching NACA0012 airfoil. Assuming an unstretched …

In the present work, we studied numerical and experimentally analysis lift and drag
performances of NACA 0015 airfoil at different attack angle at low Reynolds numbers (Re) …

The focus of this work is to dissect the physical mechanisms that drive and sustain flow-
induced, transverse vibrations of cylinders. The influence of different mechanisms is …

Due to the strong nonlinear properties of the entire flutter process including growth stages,
decay stages and steady limit cycle oscillations (LCOs), the generalization of the self-excited …

The flight of many birds and bats, and their robotic counterparts, occurs over a range of
chord-based Reynolds numbers from 1× 104 to 1.5× 105. It is precisely over this range …

Dynamic mode decomposition (DMD) has proven to be a valuable tool for the analysis of
complex flow-fields but the application of this technique to flows with moving boundaries is …

This paper investigates the potential of using an active flow control technique to modify stall
flutter oscillations of a NACA (National Advisory Committee for Aeronautics) 0015 wing …