Add to ORKGMathematical model of stability loss due to flutter effect.The origin of instability consists of nonconservative andgyroscopic forces
This paper investigates the effect of model uncertainty on the nonlinear dynamics of a generic aeroe...
The objective of this work is to investigate the dynamic behaviour of aero-elastic vibrations in the...
Stability of a linear autonomous non-conservative system in the presence of potential, gyroscopic, d...
Oscillations of a purely gyrostatic system with two degrees of freedom are constituted by elliptic p...
Abstract This paper discusses the modeling and stability analysis of aero elastic system. Aero elast...
The effect of non-linearities, be they structural, aerodynamic or control, on the aeroelastic behavi...
Flutter is an aerolastic phenomenon that makes structures oscillate when surrounded by a moving flui...
The Peters model is used to simulate the linear aerodynamic force and ONERA stall model is used to s...
This work gives a complete overview on the subject of nonconservative stability from the modern poin...
SUMMARY: Flutter instability in an infinite medium is a form of material instability corresponding t...
Gyroscopic stabilization of a linear conservative system, which is statically unstable, can be eithe...
International audienceThis monograph gives a complete overview on the subject of nonconservative sta...
This paper is concerned primarily with the analysis and resolution of the problems and contradiction...
Robust flutter analysis deals with aeroelastic (or aeroservoelastic) stability analysis taking struc...
Experience has shown that aircraft structures are generally affected by structural nonlinearities. T...
This paper investigates the effect of model uncertainty on the nonlinear dynamics of a generic aeroe...
The objective of this work is to investigate the dynamic behaviour of aero-elastic vibrations in the...
Stability of a linear autonomous non-conservative system in the presence of potential, gyroscopic, d...
Oscillations of a purely gyrostatic system with two degrees of freedom are constituted by elliptic p...
Abstract This paper discusses the modeling and stability analysis of aero elastic system. Aero elast...
The effect of non-linearities, be they structural, aerodynamic or control, on the aeroelastic behavi...
Flutter is an aerolastic phenomenon that makes structures oscillate when surrounded by a moving flui...
The Peters model is used to simulate the linear aerodynamic force and ONERA stall model is used to s...
This work gives a complete overview on the subject of nonconservative stability from the modern poin...
SUMMARY: Flutter instability in an infinite medium is a form of material instability corresponding t...
Gyroscopic stabilization of a linear conservative system, which is statically unstable, can be eithe...
International audienceThis monograph gives a complete overview on the subject of nonconservative sta...
This paper is concerned primarily with the analysis and resolution of the problems and contradiction...
Robust flutter analysis deals with aeroelastic (or aeroservoelastic) stability analysis taking struc...
Experience has shown that aircraft structures are generally affected by structural nonlinearities. T...
This paper investigates the effect of model uncertainty on the nonlinear dynamics of a generic aeroe...
The objective of this work is to investigate the dynamic behaviour of aero-elastic vibrations in the...
Stability of a linear autonomous non-conservative system in the presence of potential, gyroscopic, d...