Damping induced by vertically sloshing liquids at large amplitudes is of interest in the understanding of the dynamic response of aircraft wings containing fuel. This work presents the experimental investigation of sloshinginduced damping in two small rectangular tanks (L = 100 mm, h = 37.5 mm and 50 mm) under vertical excitation at various frequencies (3.3 to 10.3 Hz) and amplitudes (up to 1.57 tank heights). The focus is placed on large amplitudes that lead to violent vertical interactions between the liquid and the tank and the nonlinear damping effects they cause. The sloshing-induced dissipative energy in dimensional form shows a deviation from linearity with increasing amplitude of excitation, which is attributed to force-displacement...
Fuel sloshing-induced damping is currently being studied extensively within the EU-funded SLOWD proj...
Fuel sloshing inside aircraft wing tanks is not currently considered as a means of passive loads all...
All aircraft are subjected to dynamics loads resulting from in-flight atmospheric gusts and turbulen...
An investigation was performed to measure sloshing motion and damping during harmonic forced vertica...
The effort to reduce costs and environmental impact of modern commercial aircraft requires an ever b...
Violent and vertical sloshing flows appear when the fuel tanks of aircraft wings are shaken by air g...
The effort to reduce costs and environmental impact of modern commercial aircraft requires an ever b...
All aircraft are subject to a range of loading throughout ground and flight operations, which ultima...
Vertical sloshing of liquid-filled tanks has been shown to induce substantial dissipative effects. B...
: The added damping generated by liquid sloshing in a tank has been utilized in a number of civil ap...
Fuel sloshing inside aircraft wings can potentially increase the net damping of the wing structure. ...
The analysis of violent sloshing is of great interest for European aeroplane manufacturers. It has b...
The sloshing motion of a confined liquid inside a vertically moving tank is analyzed in the present ...
A dynamical system involving the decaying test of a partially filled liquid tank is analyzed in the ...
The effect of the sloshing motion of liquid in a tank on the vertical transient motion of a single d...
Fuel sloshing-induced damping is currently being studied extensively within the EU-funded SLOWD proj...
Fuel sloshing inside aircraft wing tanks is not currently considered as a means of passive loads all...
All aircraft are subjected to dynamics loads resulting from in-flight atmospheric gusts and turbulen...
An investigation was performed to measure sloshing motion and damping during harmonic forced vertica...
The effort to reduce costs and environmental impact of modern commercial aircraft requires an ever b...
Violent and vertical sloshing flows appear when the fuel tanks of aircraft wings are shaken by air g...
The effort to reduce costs and environmental impact of modern commercial aircraft requires an ever b...
All aircraft are subject to a range of loading throughout ground and flight operations, which ultima...
Vertical sloshing of liquid-filled tanks has been shown to induce substantial dissipative effects. B...
: The added damping generated by liquid sloshing in a tank has been utilized in a number of civil ap...
Fuel sloshing inside aircraft wings can potentially increase the net damping of the wing structure. ...
The analysis of violent sloshing is of great interest for European aeroplane manufacturers. It has b...
The sloshing motion of a confined liquid inside a vertically moving tank is analyzed in the present ...
A dynamical system involving the decaying test of a partially filled liquid tank is analyzed in the ...
The effect of the sloshing motion of liquid in a tank on the vertical transient motion of a single d...
Fuel sloshing-induced damping is currently being studied extensively within the EU-funded SLOWD proj...
Fuel sloshing inside aircraft wing tanks is not currently considered as a means of passive loads all...
All aircraft are subjected to dynamics loads resulting from in-flight atmospheric gusts and turbulen...