The split velocity method was applied to study the response of a finite flat-plate wing with an
aspect ratio of four encountering a large transverse gust with various gust widths. The gust is …

Active gust load alleviation techniques exhibit a high potential in significantly reducing the
transient gust loads on aircraft. In this work the aerodynamic potential of trailing-edge flaps …

As the desire for more flexible aircraft structures increases, so does the need to incorporate
the intrinsic nonlinearities in their aeroelastic analyses. In that manner, it becomes essential …

This study presents an investigation of the aerodynamic damping of light dynamic stall
phenomena on a pitching NACA 0012 airfoil via Dynamic Modal Decomposition (DMD) and …

An analytical and computational investigation of the effect of control surface freeplay on
aeroelastic behavior, including random gust response and limit cycle oscillations (LCO), is …

High-aspect-ratio (AR) wings are the prominent feature of very flexible aircraft, and greater
AR designs are being explored for enhanced flight efficiency in civil aviation. However, the …

This paper presents a kriging-based methodology for analyzing aeroelastic gust responses
at high angles of attack. Linear analysis becomes inaccurate due to the flow separation at …

Understanding the aerodynamics of multi-rotor systems under temporally varying discrete
gusts is the focus of this work. Axial and edgewise 1-minus-cosine profiles of varying …

Large-amplitude excitations need to be considered for gust load analyses of transport
aircraft in cruise flight conditions. Nonlinear amplitude effects in transonic flow are, however …

In recent years, there has been a growing interest in unmanned aerial vehicle (UAV)
configurations that fly at low airspeed [1–4]. It was observed that atmospheric gusts are …