Add to ORKGFlutter simulation of a transonic wing has been presented using a moving grid system. At first, a Navier-Stokes code has been validated by comparing computed solutions with experimental data for the oscillatory motion of rectangular wing. Then, flutter simulation of a high-aspect-ratio swept back wing has been presented. Aeroelastic responses are computed using the modal analysis based on the finite-element method. The computed flutter boundaries are obtained and compared with NAL (National Aerospace Laboratory) flutter tunnel test
An integrated computational uid dynamics (CFD) and computational structural dynamics (CSD) method i...
All flying vehicles are not stiff enough, and its flexibility can interact with the flow around it t...
Aeroelastic phenomena such as flutter can have a detrimental effect on aircraft performance and can ...
To a kind of full aircraft flutter which is called bend-bend coupling flutter, mass parameter is sig...
For an accurate prediction of the steady and unsteady behaviour of an aircraft it is necessary to ta...
Aerodynamic simulations were performed in order to compute the unsteady load response of the NLR 730...
A Navier-Stokes Computational Fluid Dynamics (CFD) code is coupled with a Computa-tional Structural ...
In order to investigate aeroelastic aspects of engine/airframe integration, a simulation chain is se...
Three different levels of unsteady CFD methods are used for transonic aeroelastic computations at DL...
© 2019 by Max Opgenoord, Mark Drela, and Karen Willcox. Transonic aeroelasticity is an important con...
The flutter characteristics of the first AGARD standard aeroelastic configuration for dynamic respon...
Transonic aeroelastic analysis at the design level relies on linear panel methods, such as the Doubl...
Abstract. The development of a methodology for determining the flutter conditions of supercritical w...
An integrated Computational Fluid Dynamics (CFD) and Computational Structural Dynamics (CSD) method ...
Calculating the flutter boundary by solving the Reynolds averaged Navier Stokes (RANS) equations in ...
An integrated computational uid dynamics (CFD) and computational structural dynamics (CSD) method i...
All flying vehicles are not stiff enough, and its flexibility can interact with the flow around it t...
Aeroelastic phenomena such as flutter can have a detrimental effect on aircraft performance and can ...
To a kind of full aircraft flutter which is called bend-bend coupling flutter, mass parameter is sig...
For an accurate prediction of the steady and unsteady behaviour of an aircraft it is necessary to ta...
Aerodynamic simulations were performed in order to compute the unsteady load response of the NLR 730...
A Navier-Stokes Computational Fluid Dynamics (CFD) code is coupled with a Computa-tional Structural ...
In order to investigate aeroelastic aspects of engine/airframe integration, a simulation chain is se...
Three different levels of unsteady CFD methods are used for transonic aeroelastic computations at DL...
© 2019 by Max Opgenoord, Mark Drela, and Karen Willcox. Transonic aeroelasticity is an important con...
The flutter characteristics of the first AGARD standard aeroelastic configuration for dynamic respon...
Transonic aeroelastic analysis at the design level relies on linear panel methods, such as the Doubl...
Abstract. The development of a methodology for determining the flutter conditions of supercritical w...
An integrated Computational Fluid Dynamics (CFD) and Computational Structural Dynamics (CSD) method ...
Calculating the flutter boundary by solving the Reynolds averaged Navier Stokes (RANS) equations in ...
An integrated computational uid dynamics (CFD) and computational structural dynamics (CSD) method i...
All flying vehicles are not stiff enough, and its flexibility can interact with the flow around it t...
Aeroelastic phenomena such as flutter can have a detrimental effect on aircraft performance and can ...