An integrated nonlinear approach for turbomachinery forced response prediction. Part I: Formulation

This paper describes the formulation of an advanced numerical model for the simulation of high- and low-engine-order forced response for turbomachiner y applications. The various forced response mechanisms are explained in som e detail and a specification for an accurate prediction system is discussed with emphasis on both fluid and structural modelling aspects. The Favre-av eraged Navier-Stokes equations are used to represent the unsteady flow in a nonlinear time-accurate fashion. Features such as turbulence modelling, bo undary conditions, meshing strategies and numerical treatments are discusse d in detail. The structural model is based on a linear modal model, though local nonlinearities due friction dampers can be accommodated using an iter ative scheme. The fluid mesh is moved at each-time step according to the st ructural motion, so that changes in blade aerodynamic damping and flow unst eadiness can be accommodated. It is concluded that the model can be used fo r large simulations involving multi-bladerow whole-annulus calculations. (C ) 2000 Academic Press.