Towards long length scale unsteady modelling in turbomachines

Abstract The modelling issue of long length scale unsteadiness in turbomachines is discussed in this paper and a new three-dimensional CFD method with a hierarchy of body force models is proposed. A program has been developed to deal with the long length scale problem using efficient coarse meshes and large time steps, together with body force models. The distributed viscous body force can be calculated either using a very simple viscous wall shear stress model or extracted from a ‘stand-alone’ three-dimensional single passage steady calculation using a fine mesh. By eliminating the need to compute fine viscous scales, the proposed method is several orders of magnitude more efficient than ‘standard’ fine mesh N-S unsteady calculations while maintaining respectable resolution down to the scale of blade-to-blade variation, including wake/potential interactions between blade rows. Two sample cases with high-frequency low-amplitude and low-frequency high-amplitude, respectively, are used to illustrate the accuracy of the model.

[1]  Milt Davis A Stage-by-Stage Dual-Spool Compression System Modeling Technique , 1982 .

[2]  E. Greitzer,et al.  A Method for Assessing Effects of Circumferential Flow Distortion on Compressor Stability , 1987 .

[3]  L. He,et al.  Method of Simulating Unsteady Turbomachinery Flows with Multiple Perturbations , 1992 .

[4]  V. Garnier,et al.  Numerical simulations of surge and rotating-stall in multi-stage axial-flow compressors , 1994 .

[5]  J. P. Longley Calculating the Flowfield Behaviour of High-Speed Multi-Stage Compressors , 1997 .

[6]  Tom Hynes,et al.  The simulation of turbomachinery blade rows in asymmetric flow using actuator disks , 1997 .

[7]  C. Hah,et al.  Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor , 1998 .

[8]  Edward M. Greitzer,et al.  A Computational Model for Short Wavelength Stall Inception and Development in Multi-Stage Compressors , 1998 .

[9]  E. M. Greitzer,et al.  A Computational Model for Short-Wavelength Stall Inception and Development in Multistage Compressors , 1999 .

[10]  Juan J. Alonso,et al.  Development and validation of a massively parallel flow solver for turbomachinery flows , 2000 .

[11]  John D. Denton,et al.  Prediction of Low Engine Order Inlet Distortion Driven Resonance in a Low Aspect Ratio Fan , 2000 .

[12]  L. He,et al.  Single-passage solution of three-dimensional unsteady flows in a transonic fan rotor , 2001 .

[13]  John D. Denton,et al.  The Effects of Lean and Sweep on Transonic Fan Performance , 2002 .