论文信息 - A non-linear integrated aeroelasticity method for the prediction of turbine forced response with friction dampers - 字舞流文

A non-linear integrated aeroelasticity method for the prediction of turbine forced response with friction dampers

An integrated aeroelasticity model was described for turbine blade forced response predictions. An iterative procedure was developed to determine the resonance shift under the effects of both unste ...

C. Breard | Mehdi Vahdati | Mehmet Imregun | James Green

[1] Michael B. Giles,et al. Calculation of Unsteady Wake/Rotor Interaction , 1987 .

[2] Man Mohan Rai,et al. Navier-Stokes Simulations of Rotor/Stator Interaction Using Patched and Overlaid Grids , 1987 .

[3] Abdulnaser I. Sayma,et al. Semi-structured meshes for axial turbomachinery blades , 2000 .

[4] Abdulnaser I. Sayma,et al. AN INTEGRATED NONLINEAR APPROACH FOR TURBOMACHINERY FORCED RESPONSE PREDICTION. PART II: CASE STUDIES , 2000 .

[5] Wagdi G. Habashi,et al. Solution techniques for large-scale CFD problems , 1995 .

[6] William N. Dawes. Development of a 3D Navier Stokes Solver for Application to all Types of Turbomachinery , 1988 .

[7] David J. Ewins,et al. MODELLING TWO-DIMENSIONAL FRICTION CONTACT AND ITS APPLICATION USING HARMONIC BALANCE METHOD , 1996 .

[8] Abdulnaser I. Sayma,et al. AN INTEGRATED NONLINEAR APPROACH FOR TURBOMACHINERY FORCED RESPONSE PREDICTION. PART I: FORMULATION , 2000 .

[9] M. Imregun,et al. An Analysis of the Aeroelastic Behaviour of a Typical Fan-Blade With Emphasis on the Flutter Mechanism , 1996 .

[10] Abdulnaser I. Sayma,et al. Modeling of Three-Dimensional Viscous Compressible Turbomachinery Flows Using Unstructured Hybrid Grids , 2000 .

[11] T. Barth,et al. A one-equation turbulence transport model for high Reynolds number wall-bounded flows , 1990 .