Add to ORKGIn this study, a comparison study of flutter analysis for the AGARD 445.6 wing with wind turnnel test data has been conducted in the subsonic, transonic and supersonic flow regions. Nonlinear aeroelastic using FSIPRO3D which is a generalized user-friendly fluid-structure analyses have been conducted for a 3D wing configuration considering shockwave and turbulent viscosity effects. The developed fluid-structure coupled analysis system is applied for aeroelastic computations combining computational structure dynamics(CSD), finite element method(FEM) and computations fluid dynamics(CFD) in the time domain. MSC/NASTRAN is used for the vibration analysis of a wing model, and then the result is applied to the FSIPRO3D module. the results for dyna...
To a kind of full aircraft flutter which is called bend-bend coupling flutter, mass parameter is sig...
An integrated computational fluid dynamics and computational structural dynamics (CFD-CSD) approach ...
Transonic aeroelastic analysis at the design level relies on linear panel methods, such as the Doubl...
The flutter characteristics of the first AGARD standard aeroelastic configuration for dynamic respon...
For an accurate prediction of the steady and unsteady behaviour of an aircraft it is necessary to ta...
A method based on the Euler equations is proposed for solving transonic flutter problems. The transo...
This paper builds on the computational aeroelastic results published previously and generated in sup...
To promote the evaluation of existing and emerging unsteady aerodynamic codes and methods for applyi...
Through the coupling between aerodynamic and structural governing equations, a fully implicit multib...
A Navier-Stokes Computational Fluid Dynamics (CFD) code is coupled with a Computa-tional Structural ...
This paper gives an overview of the numerical procedures which are nowadays used at Dipartimento di ...
An integrated Computational Fluid Dynamics (CFD) and Computational Structural Dynamics (CSD) method ...
An integrated computational uid dynamics (CFD) and computational structural dynamics (CSD) method i...
The development of advanced-design ultrahigh bypass ratio engines has led to renewed interest in the...
A partitioned fluid–structure coupling code for transonic panel flutter has been developed and valid...
To a kind of full aircraft flutter which is called bend-bend coupling flutter, mass parameter is sig...
An integrated computational fluid dynamics and computational structural dynamics (CFD-CSD) approach ...
Transonic aeroelastic analysis at the design level relies on linear panel methods, such as the Doubl...
The flutter characteristics of the first AGARD standard aeroelastic configuration for dynamic respon...
For an accurate prediction of the steady and unsteady behaviour of an aircraft it is necessary to ta...
A method based on the Euler equations is proposed for solving transonic flutter problems. The transo...
This paper builds on the computational aeroelastic results published previously and generated in sup...
To promote the evaluation of existing and emerging unsteady aerodynamic codes and methods for applyi...
Through the coupling between aerodynamic and structural governing equations, a fully implicit multib...
A Navier-Stokes Computational Fluid Dynamics (CFD) code is coupled with a Computa-tional Structural ...
This paper gives an overview of the numerical procedures which are nowadays used at Dipartimento di ...
An integrated Computational Fluid Dynamics (CFD) and Computational Structural Dynamics (CSD) method ...
An integrated computational uid dynamics (CFD) and computational structural dynamics (CSD) method i...
The development of advanced-design ultrahigh bypass ratio engines has led to renewed interest in the...
A partitioned fluid–structure coupling code for transonic panel flutter has been developed and valid...
To a kind of full aircraft flutter which is called bend-bend coupling flutter, mass parameter is sig...
An integrated computational fluid dynamics and computational structural dynamics (CFD-CSD) approach ...
Transonic aeroelastic analysis at the design level relies on linear panel methods, such as the Doubl...