The paper describes the flutter stability assessment of a steam turbine rotor and the application of a multi-disciplinary shape optimization procedure to obtain a new blade geometry with higher efficiency and an improved flutter stability. The investigated test case consists of a steam turbine last stage representative of modern industrial steam turbine blading, firstly presented by Durham University and intensively investigated during last years. The aerodamping results on the original geometry, obtained by a non-linear method, are compared with those already published by other researches with different flutter approaches. The present results are in complete agreement with numerical investigations already present in the literature and show a high blade instability for the first bending mode. Starting from this unstable geometry, a shape optimization procedure with aeromechanical constraints has been applied in order to obtain a blade with improved performances from both the aerodynamic and the flutter point of view. The optimum profile shows a higher efficiency and a flutter instability reduction. Those aspects are exhaustively discussed and comparisons with the baseline geometry are reported. KEYWORDSCFD, FLUTTER, OPTIMIZATION, STEAM TURBINE NOMENCLATURE ṁ mass flow p pressure Greek: η T T total-to-total stage efficiency ω * reduced frequency, = ω * c/v out σ static stress ξ logarithmic decrement (log.dec.
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.
hi@scite.ai
10624 S. Eastern Ave., Ste. A-614
Henderson, NV 89052, USA
Copyright © 2024 scite LLC. All rights reserved.
Made with 💙 for researchers
Part of the Research Solutions Family.