Three model-motions were developed to replicate the aerodynamic response of a transverse gust. These motions included a pure-plunging and two three degree-of-freedom motions that approximated the angle-of-attack distribution produced by the gust. Using inviscid models and viscous flow simulations, the response of the gust and model-motions were compared as a function of the non-dimensional reduced frequency. The inviscid model was found to overestimate the influence of the rotational added-mass in the three degree-of-freedom motions. In contrast, the viscous flow simulations showed that the two primary sources of discrepancy between the gust and model-motions lie in the non-linear angle-of-attack distribution caused by the gust, and the wak...
The stresses resulting from wind gusts can exceed the limit value and may cause large-scale structur...
The aeroelastic response of an airfoil featuring plunging-pitching coupled motion in an incompressib...
The emerging design of MAVs has arisen a great interest in making research about unsteady Aerodynam...
The flow field and force produced during a wing-gust encounter have been compared between a top-hat ...
Extreme atmospheric conditions can affect the stability of aerial vehicles that, consequently, requi...
The small size and low speed of Micro Air Vehicles make them vulnerable to wind gusts such that sust...
A large variety of gusts that develop in the atmospheric boundary layer affect aerial vehicles. This...
This paper studies and compares the effects of transverse and vortex gust encounters. A sine-squared...
Small unmanned aerial vehicles and biological fliers can experience wind gusts of similar magnitude ...
Longitudinally gusting ow over a nominally two dimensional airfoil is exam- ined over a range of inc...
Gust analysis is one key task during design and certification of new aircraft. In the industrial sta...
Based on Navier-Stokes equations and structural and flight dynamic equations of motion, dynamic resp...
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. To aid th...
As part of an effort to examine the impact of vortical gusts on airfoils, a simple gust generator h...
This thesis examines two methods of vortical gust generation and the interaction between these gusts...
The stresses resulting from wind gusts can exceed the limit value and may cause large-scale structur...
The aeroelastic response of an airfoil featuring plunging-pitching coupled motion in an incompressib...
The emerging design of MAVs has arisen a great interest in making research about unsteady Aerodynam...
The flow field and force produced during a wing-gust encounter have been compared between a top-hat ...
Extreme atmospheric conditions can affect the stability of aerial vehicles that, consequently, requi...
The small size and low speed of Micro Air Vehicles make them vulnerable to wind gusts such that sust...
A large variety of gusts that develop in the atmospheric boundary layer affect aerial vehicles. This...
This paper studies and compares the effects of transverse and vortex gust encounters. A sine-squared...
Small unmanned aerial vehicles and biological fliers can experience wind gusts of similar magnitude ...
Longitudinally gusting ow over a nominally two dimensional airfoil is exam- ined over a range of inc...
Gust analysis is one key task during design and certification of new aircraft. In the industrial sta...
Based on Navier-Stokes equations and structural and flight dynamic equations of motion, dynamic resp...
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. To aid th...
As part of an effort to examine the impact of vortical gusts on airfoils, a simple gust generator h...
This thesis examines two methods of vortical gust generation and the interaction between these gusts...
The stresses resulting from wind gusts can exceed the limit value and may cause large-scale structur...
The aeroelastic response of an airfoil featuring plunging-pitching coupled motion in an incompressib...
The emerging design of MAVs has arisen a great interest in making research about unsteady Aerodynam...