A time-marching coupled method has been applied to a high pressure compressor forced response case. The purpose of the study is to compare the contribution of the coupled scheme against the state of the art decoupled methodology. Although the time-marching scheme allows for a stronger coupling between the motion and aerodynamic field, results have shown good agreement with the decoupled method. The additional computing cost arising from the long transient state and the small difference in amplitude prediction with the decoupled scheme reduce the interest for the coupled one. A new transient state method is proposed to combine both coupled and decoupled schemes features. Here, the forcing and damping functions are extracted during the mechanical transient state of the coupled simulation and forced response is calculated as in the decoupled method. Results have shown good agreements with the experiment and all the methods are compared in terms of underlying assumptions and performances.
Skip Nav Destination
ASME 2012 Gas Turbine India Conference
December 1, 2012
Mumbai, Maharashtra, India
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4516-5
PROCEEDINGS PAPER
Comparison of Fluid-Structure Coupling Methods for Blade Forced Response Prediction
Florent Payer,
Florent Payer
Snecma (Safran Group), Villaroche, France
Search for other works by this author on:
Pascal Ferrand,
Pascal Ferrand
Ecole Centrale de Lyon, Ecully, France
Search for other works by this author on:
Fabrice Thouverez
Fabrice Thouverez
Ecole Centrale de Lyon, Ecully, France
Search for other works by this author on:
Florent Payer
Snecma (Safran Group), Villaroche, France
Pascal Ferrand
Ecole Centrale de Lyon, Ecully, France
Alain Dugeai
ONERA, Chatillon, France
Fabrice Thouverez
Ecole Centrale de Lyon, Ecully, France
Paper No:
GTINDIA2012-9521, pp. 595-602; 8 pages
Published Online:
July 25, 2013
Citation
Payer, F, Ferrand, P, Dugeai, A, & Thouverez, F. "Comparison of Fluid-Structure Coupling Methods for Blade Forced Response Prediction." Proceedings of the ASME 2012 Gas Turbine India Conference. ASME 2012 Gas Turbine India Conference. Mumbai, Maharashtra, India. December 1, 2012. pp. 595-602. ASME. https://doi.org/10.1115/GTINDIA2012-9521
Download citation file:
22
Views
Related Proceedings Papers
Related Articles
Impact of Manufacturing Variability and Nonaxisymmetry on High-Pressure Compressor Stage Performance
J. Eng. Gas Turbines Power (March,2012)
Multibladerow Forced Response Modeling in Axial-Flow Core Compressors
J. Turbomach (April,2007)
The Cumulative Effects of Forcing Function, Damping, and Mistuning on Blade Forced Response in a High Speed Centrifugal Compressor With Inlet Distortion
J. Eng. Gas Turbines Power (December,2010)
Related Chapters
Stability and Range
Design and Analysis of Centrifugal Compressors
Introduction to Pipeline Systems
Pipeline Pumping and Compression Systems: A Practical Approach
Combined Cycle Power Plant
Energy and Power Generation Handbook: Established and Emerging Technologies