0
TECHNICAL PAPERS: Gas Turbines: Combustion and Fuels

On the Use of Helmholtz Resonators for Damping Acoustic Pulsations in Industrial Gas Turbines

[+] Author and Article Information
V. Bellucci, P. Flohr

ALSTOM (Switzerland) Ltd., Im Segelhof 1, CH-5405 Baden-Dättwil, Switzerland

C. O. Paschereit

Technical University of Berlin, D-10623 Berlin, Germanye-mail: oliver.paschereit@tu-berlin.de

F. Magni

ALSTOM (Switzerland) Ltd., Haselstrasse 16, CH-5401 Baden, Switzerlande-mail: fulvio.magni@power.alstom.com

J. Eng. Gas Turbines Power 126(2), 271-275 (Jun 07, 2004) (5 pages) doi:10.1115/1.1473152 History: Received December 01, 2000; Revised March 01, 2001; Online June 07, 2004
Copyright © 2002 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
g(x)-function of nonlinear pressure loss
Grahic Jump Location
Relative attenuation for Case A
Grahic Jump Location
Combustor eigenmode at St=0.6
Grahic Jump Location
Measured versus computed pressure spectrum without resonators
Grahic Jump Location
Measured versus computed pressure spectrum with resonators

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In