Add to ORKGAbstract. A multiblock method is presented for the solution of a three di-mensional model of aeroelasticity in a turbomachine blade row. The method employs a fully coupled approach and the structural model involves modal reduction. Transnite interpolation is used to adapt the uid grid to the moving structure. 1
This work provides an accurate and efficient numerical method for turbomachinery flutter. The unstea...
SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92871) / BLDSC - British Lib...
ABSTRACT A three-dimensional nonlinear time-marching method and numerical analysis for aeroelastic b...
A numerical method for the computation of aeroelasticity is presented. Although the emphasis here is...
This work provides an extension to 3D aeroelastic problems of a recently developed numerical method ...
Under this grant, Version 4 of the three-dimensional Navier-Stokes aeroelastic code (TURBO-AE) has b...
In turbomachinery, the continuous drive towards low weight and improved efficiency has led to the de...
This paper describes an aeroelastic analysis program for turbomachines. Unsteady Navier-Stokes equat...
rou ati r t ea g ion th uta ary Although experimental studies play an important role in the research...
A reduced order aerodynamic model is developed for aeroelastic analysis of turbomachines. The proper...
This study presents an approach based on the floating frame of reference method to model complex thr...
Communication to : AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit, Monterey, CA (US...
We present the development and validation of a parallel unsteady flow and aeroelasticity code for la...
A multiple multigrid method for the solution of the 3-D Euler and Navier-Stokes equations is present...
A parallel multi-block Navier-Stokes solver with the k-ω turbulence model is developed to simulate t...
This work provides an accurate and efficient numerical method for turbomachinery flutter. The unstea...
SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92871) / BLDSC - British Lib...
ABSTRACT A three-dimensional nonlinear time-marching method and numerical analysis for aeroelastic b...
A numerical method for the computation of aeroelasticity is presented. Although the emphasis here is...
This work provides an extension to 3D aeroelastic problems of a recently developed numerical method ...
Under this grant, Version 4 of the three-dimensional Navier-Stokes aeroelastic code (TURBO-AE) has b...
In turbomachinery, the continuous drive towards low weight and improved efficiency has led to the de...
This paper describes an aeroelastic analysis program for turbomachines. Unsteady Navier-Stokes equat...
rou ati r t ea g ion th uta ary Although experimental studies play an important role in the research...
A reduced order aerodynamic model is developed for aeroelastic analysis of turbomachines. The proper...
This study presents an approach based on the floating frame of reference method to model complex thr...
Communication to : AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit, Monterey, CA (US...
We present the development and validation of a parallel unsteady flow and aeroelasticity code for la...
A multiple multigrid method for the solution of the 3-D Euler and Navier-Stokes equations is present...
A parallel multi-block Navier-Stokes solver with the k-ω turbulence model is developed to simulate t...
This work provides an accurate and efficient numerical method for turbomachinery flutter. The unstea...
SIGLEAvailable from British Library Document Supply Centre-DSC:8019.322(92871) / BLDSC - British Lib...
ABSTRACT A three-dimensional nonlinear time-marching method and numerical analysis for aeroelastic b...