Journal article
Fourier methods for turbomachinery applications
- Abstract:
- Rapid increase in computing power has made a huge difference in scales and complexities of the problems in turbomachinery that we can tackle by use of computational fluid dynamics (CFD). It is recognised, however, that there is always a need for developing efficient methods for applications to blade designs. In a design cycle, a large number of flow solutions are sought to interact iteratively or concurrently with various options, opportunities and constraints from other disciplines. This basic requirement for fast prediction methods in a multi-disciplinary design environment remains unchanged, regardless of computer speed. And it must be recognised that the multi-disciplinary nature of blading design increasingly influences outcomes of advanced gas turbine and aeroengine developments. Recently there has been considerable progress in the Fourier harmonic modelling method development for turbomachinery applications. The main driver is to develop efficient and accurate computational methodologies and working methods for prediction and analysis of unsteady effects on aerothermal performance (loading and efficiency) and aeroelasticity (blade vibration due to flutter and forced response) in turbomachinery. In this article, the developments and applications of this type of methods in the past 20 years or so are reviewed. The basic modelling assumptions and various forms of implementations for the temporal Fourier modelling approach are presented and discussed. Computational examples for realistic turbomachinery configurations/flow conditions are given to illustrate the validity and effectiveness of the approach. Although the major development has been in the temporal Fourier harmonic modelling, some recent progress in use of the spatial Fourier modelling is also described with demonstration examples.
- Publication status:
- Published
- Peer review status:
- Peer reviewed
Actions
Authors
+ Rolls-Royce (United Kingdom)
More from this funder
- Funder identifier:
- https://ror.org/04h08p482
- Programme:
- Chair in Computational Aerothermal Engineering at Oxford
- Publisher:
- Elsevier
- Journal:
- Progress in Aerospace Sciences More from this journal
- Volume:
- 46
- Issue:
- 8
- Pages:
- 329-341
- Publication date:
- 2010-06-10
- DOI:
- EISSN:
-
1873-1724
- ISSN:
-
0376-0421
- Language:
-
English
- Pubs id:
-
pubs:97309
- UUID:
-
uuid:a3ea5a6b-e199-4120-8965-7a512e2d40e5
- Local pid:
-
pubs:97309
- Source identifiers:
-
97309
- Deposit date:
-
2013-11-16
Terms of use
- Copyright holder:
- Elsevier Ltd
- Copyright date:
- 2010
- Rights statement:
- © 2010 Elsevier Ltd. All rights reserved.
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