Towards a reduction of compressor blade dynamic loading by means of rotor-stator interaction optimization
2002 (English)In: Proceedings of the ASME Turbo Expo 2002 Turbomachinery: presented at the 2002 ASME Turbo Expo, June 3 - 6, 2002, Amsterdam, the Netherlands, New York: American Society of Mechanical Engineers , 2002, Vol. 5A, 667-674 p.Conference paper (Refereed)
This paper presents a two-dimensional procedure for minimizing dynamic loading and maximizing time-averaged isentropic efficiency in multi-stage compressors. The procedure arises from the combination of an evolutionary algorithm and a CFD code in which a sliding mesh technique and a time-dependent approach are implemented enabling the study of unsteady rotor stator interaction. The method is then applied to a two-stage compressor cascade (rotor-stator-rotor-stator). The results concerning the optimal set of geometrical parameters considered for optimization (axial distances between successive cascades, circumferential clocking between stators and between rotors) are finally presented and discussed.
Place, publisher, year, edition, pages
New York: American Society of Mechanical Engineers , 2002. Vol. 5A, 667-674 p.
IdentifiersURN: urn:nbn:se:ltu:diva-35826DOI: 10.1115/GT2002-30396ScopusID: 36998411Local ID: a81b6a77-c6fe-49f0-9f5f-2415867a6325ISBN: 0-7918-3610-XOAI: oai:DiVA.org:ltu-35826DiVA: diva2:1009080
ASME Turbo Expo : 03/06/2002 - 06/06/2002
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