Due to the relative motion between adjacent blade rows the aerodynamic flow fields within turbomachinery are usually dominated by deterministic, periodic phenomena. In the numerical simulation of such unsteady flows, (nonlinear) frequency-domain methods are therefore attractive as they are capable of fully exploiting the given spatial and temporal periodicity, as well as modelling flow nonlinearities. A nontrivial issue in the application of frequency-domain methods to turbomachinery flows is to simultaneously capture disturbances with multiple fundamental frequencies in one relative system. In case of harmonically related frequencies, the interval spanned by the sampling points typically resolves the common fundamental frequency. To avoid signal aliasing the highest harmonic of the common frequency should be sampled with an appropriate number of sampling points. However, when the common fundamental frequency is very low in relation to the frequencies of primary interest, equidistant time sampling leads to a high number of sampling points, hence frequency-domain methods can become computationally inefficient. Furthermore, when a problem can no longer be described by harmonic perturbations that are integer multiples of one fundamental frequency, as it may occur in two-shaft configurations, the standard discrete Fourier transform is no longer suitable and the basic harmonic balance method requires extension. In this article two nonlinear frequency-domain approaches for dealing with the accounted issues are demonstrated and compared. The first approach is a generalized harmonic balance method based on almost periodic Fourier transforms with non-equidistant time sampling. Then the so-called harmonic set approach, developed by the authors, is evaluated. Based on the neglection of the nonlinear, quadratic cross-coupling terms between higher harmonics of different fundamental frequencies, the harmonic set approach allows the superposition of periodic disturbances with different fundamental frequencies as well as the separated, equidistant sampling of the highest harmonic of each base frequency. The aim of this paper is to compare the computational efficiency and accuracy of the two methods and assess the impact of neglecting the quadratic cross-coupling terms.
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ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition
June 11–15, 2018
Oslo, Norway
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5101-2
PROCEEDINGS PAPER
On the Development of Harmonic Balance Methods for Multiple Fundamental Frequencies
Laura Junge,
Laura Junge
German Aerospace Center (DLR), Cologne, Germany
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Graham Ashcroft,
Graham Ashcroft
German Aerospace Center (DLR), Cologne, Germany
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Hans-Peter Kersken,
Hans-Peter Kersken
German Aerospace Center (DLR), Cologne, Germany
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Christian Frey
Christian Frey
German Aerospace Center (DLR), Cologne, Germany
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Laura Junge
German Aerospace Center (DLR), Cologne, Germany
Graham Ashcroft
German Aerospace Center (DLR), Cologne, Germany
Hans-Peter Kersken
German Aerospace Center (DLR), Cologne, Germany
Christian Frey
German Aerospace Center (DLR), Cologne, Germany
Paper No:
GT2018-75495, V02CT42A012; 16 pages
Published Online:
August 30, 2018
Citation
Junge, L, Ashcroft, G, Kersken, H, & Frey, C. "On the Development of Harmonic Balance Methods for Multiple Fundamental Frequencies." Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. Volume 2C: Turbomachinery. Oslo, Norway. June 11–15, 2018. V02CT42A012. ASME. https://doi.org/10.1115/GT2018-75495
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