Affiliation:
1. ALSTOM Power, UK Ltd., Lincoln LN5 7FD, UK
Abstract
A multistage frequency domain (time-linearized/nonlinear harmonic) Navier-Stokes unsteady flow solver has been developed for predicting unsteady flows induced by bladerow interactions. In this paper, the time-linearized option of the solver has been used to analyze unsteady flows in a subsonic turbine test stage and the DLR transonic counter-rotating shrouded propfan. The numerical accuracy and computational efficiency of the time-linearized viscous methods have been demonstrated by comparing predictions with test data and nonlinear time-marching solutions for these two test cases. It is concluded that the development of efficient frequency domain approaches enables unsteady flow predictions to be used in the design cycles to tackle aeromechanics problems.
Reference18 articles.
1. Kielb, R. E., 1999, “Aeroelasticity in Axial Flow Turbomachines,” VKI Lecture Series 1999-05, von Karman Institute for Fluid Dynamics. May 3–7.
2. Hall, K. C., and Crawley, E. F., 1989, “Calculation of Unsteady Flows in Turbomachinery Using the Linearized Euler Equations,” AIAA J., 27, No. 6No. 6.
3. Hall, K. C., Clark, W. S., and Lorence, C. B., 1994, “A Linearized Euler Analysis of Unsteady Transonic Flows in Turbomachinery,” ASME J. Turbomach., 116.
4. Holmes, D. G., and Chuang, H. A., 1993, “2D Linearized Harmonic Euler Flow Analysis for Flutter and Forced Response,” Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers, ed., H. M. Arassi, Springer-Verlag, New York, NY.
5. Montgomery, M. D., and Verdon, J. M., 1997, “A 3-D Linearized Euler Analysis for Blade Rows. Part 1: Aerodynamic and Numerical Formulations and Part II: Unsteady Aerodynamic Response Predictions,” Unsteady Aerodynamics and Aeroelasticity of Turbomachines, ed., T. H. Fransson, Kluwer Academic Publishers.
Cited by
6 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献