A simple rectangular wing-box model with varying individual rib orientations has been analysed with the interest on studying their impact on flutter and divergence instabilities. The varying rib orientations offer an alteration in bending-torsional coupling characteristics, resulting in significant effect on aeroelastic behaviour of the wing. Substantial improvement is found in comparison with the baseline and parallel ribs orientation configurations, which leads to the possibility of significant weight reduction
This paper is concerned with the aeroelastic modeling and analysis of high aspect ratio wings with l...
suMMARY An investigation has been made with the dual purpose of deter-mining the effect of two bodie...
The paper shows preliminary results of aeroelastic analyses of two half-wing models, having curved a...
A simple un-tapered wing box model was considered to illustrate an aeroelastic tailoring of varying ...
A simple rectangular wing box model with varying rib orientations has been analyzed by observing th...
Summary This paper discusses the effect of fibre orientations, composite skin lay-up, bending-torsio...
In this paper, the aeroelastic modeling and conceptual flutter analysis of a simple 2-D box wing is ...
The present paper aims to reveal the significance of rigid-body motions for the flutter mechanism of...
The aim of this paper is to present a flutter analysis of a 3D Box-Wing Aircraft (BWA) configuration...
The paper shows preliminary results of aeroelastic analyses of two half-wing models, having curved a...
In recent years, the development of lighter and more efficient transport aircraft has led to an incr...
Three related methodologies relating to the modelling and design of aero elastic aircraft structures...
Aeroelastic analyses traditionally consider the airfoil of a wing to remain rigid, only allowing def...
A framework is presented to calculate the sensitivities of static aeroelastic wing and flutter chara...
The aim of the current paper is to present a flutter analysis of a 3-D Box-Wing Aircraft (BWA) confi...
This paper is concerned with the aeroelastic modeling and analysis of high aspect ratio wings with l...
suMMARY An investigation has been made with the dual purpose of deter-mining the effect of two bodie...
The paper shows preliminary results of aeroelastic analyses of two half-wing models, having curved a...
A simple un-tapered wing box model was considered to illustrate an aeroelastic tailoring of varying ...
A simple rectangular wing box model with varying rib orientations has been analyzed by observing th...
Summary This paper discusses the effect of fibre orientations, composite skin lay-up, bending-torsio...
In this paper, the aeroelastic modeling and conceptual flutter analysis of a simple 2-D box wing is ...
The present paper aims to reveal the significance of rigid-body motions for the flutter mechanism of...
The aim of this paper is to present a flutter analysis of a 3D Box-Wing Aircraft (BWA) configuration...
The paper shows preliminary results of aeroelastic analyses of two half-wing models, having curved a...
In recent years, the development of lighter and more efficient transport aircraft has led to an incr...
Three related methodologies relating to the modelling and design of aero elastic aircraft structures...
Aeroelastic analyses traditionally consider the airfoil of a wing to remain rigid, only allowing def...
A framework is presented to calculate the sensitivities of static aeroelastic wing and flutter chara...
The aim of the current paper is to present a flutter analysis of a 3-D Box-Wing Aircraft (BWA) confi...
This paper is concerned with the aeroelastic modeling and analysis of high aspect ratio wings with l...
suMMARY An investigation has been made with the dual purpose of deter-mining the effect of two bodie...
The paper shows preliminary results of aeroelastic analyses of two half-wing models, having curved a...