Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique

A harmonic balance technique for modeling unsteady nonlinear e ows in turbomachinery is presented. The analysis exploits the fact that many unsteady e ows of interest in turbomachinery are periodic in time. Thus, the unsteady e ow conservation variables may be represented by a Fourier series in time with spatially varying coefe cients. This assumption leads to a harmonic balance form of the Euler or Navier ‐Stokes equations, which, in turn, can be solved efe ciently as a steady problem using conventional computational e uid dynamic (CFD) methods, including pseudotime time marching with local time stepping and multigrid acceleration. Thus, the method is computationally efe cient, at least one to two orders of magnitude faster than conventional nonlinear time-domain CFD simulations. Computational results for unsteady, transonic, viscous e ow in the front stage rotor of a high-pressure compressor demonstrate that even strongly nonlinear e ows can be modeled to engineering accuracy with a small number of terms retained in the Fourier series representation of the e ow. Furthermore, in some cases, e uid nonlinearities are found to be important for surprisingly small blade vibrations.

[1]  P. D. Thomas,et al.  Direct Control of the Grid Point Distribution in Meshes Generated by Elliptic Equations , 1980 .

[2]  Howard P. Hodson,et al.  An Inviscid Blade-to-Blade Prediction of a Wake-Generated Unsteady Flow , 1985 .

[3]  Max F Platzer,et al.  AGARD Manual on Aeroelasticity in Axial-Flow Turbomachines. Volume 1. Unsteady Turbomachinery Aerodynamics , 1987 .

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

[5]  Man Mohan Rai,et al.  Three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction , 1988 .

[6]  Man Mohan Rai,et al.  Three-Dimensional Navier-Stokes Simulations of Turbine Rotor-Stator Interaction; Part I1 - Results , 1989 .

[7]  Edward F. Crawley,et al.  Calculation of unsteady flows in turbomachinery using the linearized Euler equations , 1989 .

[8]  Michael B. Giles,et al.  Nonreflecting boundary conditions for Euler equation calculations , 1990 .

[9]  Dennis L. Huff,et al.  Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme , 1991 .

[10]  Michael B. Giles,et al.  An Approach for Multi-Stage Calculations Incorporating Unsteadiness , 1992 .

[11]  P. Spalart A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .

[12]  Kenneth C. Hall,et al.  Calculation of Three-Dimensional Unsteady Flows in Turbomachinery Using the Linearized Harmonic Euler Equations , 1992 .

[13]  D. Holmes,et al.  2D Linearized Harmonic Euler Flow Analysis for Flutter and Forced Response , 1993 .

[14]  Kenneth C. Hall,et al.  Linearized Euler predictions of unsteady aerodynamic loads in cascades , 1993 .

[15]  Kenneth C. Hall,et al.  Nonreflecting boundary conditions for linearized unsteady aerodynamic calculations , 1993 .

[16]  John D. Denton,et al.  Three-dimensional time-marching inviscid and viscous solutions for unsteady flows around vibrating blades , 1993 .

[17]  W. Ning,et al.  Efficient Approach for Analysis of Unsteady Viscous Flows in Turbomachines , 1998 .

[18]  Li He,et al.  Computation of unsteady flows around oscillating blades using linear and nonlinear harmonic Euler methods , 1998 .

[19]  Kenneth C. Hall,et al.  A Time-Linearized Navier-Stokes Analysis of Stall Flutter , 1999 .

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

[21]  Kenneth C. Hall,et al.  A Time-Linearized Navier–Stokes Analysis of Stall Flutter , 2000 .

[22]  Earl H. Dowell,et al.  Parametric Study of Flutter for an Airfoil in Inviscid Transonic Flow , 2003 .

[23]  Kivanc Ekici,et al.  Frequency Domain Techniques for Complex and Nonlinear Flows in Turbomachinery (Invited) , 2003 .

[24]  E. Dowell,et al.  Compact Methodology for Computing Limit-Cycle Oscillations in Aeroelasticity , 2003 .

[25]  M. Oxley,et al.  Adaptive Harmonic Balance Solutions to Euler' s Equation , 2003 .

[26]  Earl H. Dowell,et al.  Improved Understanding of Transonic Flutter: A Three-Parameter Flutter Surface , 2004 .

[27]  Jeffrey P. Thomas,et al.  Limit-Cycle Oscillations of a Typical Airfoil in Transonic Flow , 2004 .

[28]  P. Beran,et al.  Reduced-order modeling: new approaches for computational physics , 2004 .