Flutter Analysis of a Transonic Steam Turbine Blade with Frequency and Time-Domain Solvers

Author:

Frey Christian,Ashcroft Graham,Kersken Hans-Peter,Schlüß Daniel

Abstract

The aim of this study was to assess the capabilities of different simulation approaches to predict the flutter stability of a steam turbine rotor. The focus here was on linear and nonlinear frequency domain solvers in combination with the energy method, which is widely used for the prediction of flutter onset. Whereas a GMRES solver was used for the linear problem, the nonlinear methods employed a time-marching procedure. The solvers were applied to the flutter analysis of the first rotor bending mode of the open Durham Steam Turbine test case. This test case is representative of the last stage of modern industrial steam turbines. We compared our results to those published by other researchers in terms of aerodynamic damping and local work per cycle coefficients. Time-domain, harmonic balance, and time-linearised methods were compared to each other in terms of CPU efficiency and accuracy.

Publisher

MDPI AG

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering

Reference26 articles.

Cited by 10 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

1. Investigation of Blade Cascade Torsional Flutter Using the Discontinuous Galerkin Approach in Correlation with Experimental Measurements;International Journal of Computational Fluid Dynamics;2024-09-05

2. Physics guided machine learning modelling of compressor stall flutter;Journal of the Global Power and Propulsion Society;2024-08-13

3. Enhancing low-pressure stage steam turbine using the TDLD criterion and the TOPSIS analysis;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2023-11-14

4. Evaluating the Aerodynamic Damping At Shock Wave Boundary Layer Interacting Flow Conditions With Harmonic Balance;Journal of Engineering for Gas Turbines and Power;2022-12-05

5. Acoustic Feedback and Its Impact on Fan Flutter in Short Aeroengine Intakes;Journal of Propulsion and Power;2022-07

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