Imperial College London

ProfessorWilliamJones

Faculty of EngineeringDepartment of Mechanical Engineering

Professor
 
 
 
//

Contact

 

+44 (0)20 7594 7037w.jones

 
 
//

Assistant

 

Ms Fabienne Laperche +44 (0)20 7594 7033

 
//

Location

 

607City and Guilds BuildingSouth Kensington Campus

//

Summary

 

Publications

Citation

BibTex format

@inproceedings{Fredrich:2019,
author = {Fredrich, D and Jones, WP and Marquis, A},
pages = {1--12},
publisher = {The Combustion Institute},
title = {Thermo-acoustic instabilities in the PRECCINSTA combustor investigated using a compressible LES-pdf approach},
url = {http://hdl.handle.net/10044/1/84615},
year = {2019}
}

RIS format (EndNote, RefMan)

TY  - CPAPER
AB - This work predicts the evolution of self-excited thermo-acoustic instabilities in a gas turbine model combustor using large eddy simulation. The developed flow solver is fully compressible and comprises a transported sub-grid probability density function approach in conjunction with the Eulerian stochastic fields method. An unstable operating condition in the PREC-CINSTA test case involving flame oscillation driven by thermo-acoustic instabilities is the chosen target configuration. Good results are obtained in a comparison of time-averaged flow statistics against experimental data. The flame’s self-excited oscillatory behaviour is successfully captured without any external forcing involved. Power spectral density analysis of the oscillation reveals a dominant thermo-acoustic mode at a frequency of 300 Hz providing remarkable agreement with experimental observations. Moreover, the predicted limit-cycle amplitude closely matches the experimental value obtained with rigid metal combustion chamber side walls. Finally, a phase-resolved study of the oscillation cycle is carried out leading to a detailed description of the physical mechanism closing the feedback loop.
AU - Fredrich,D
AU - Jones,WP
AU - Marquis,A
EP - 12
PB - The Combustion Institute
PY - 2019///
SP - 1
TI - Thermo-acoustic instabilities in the PRECCINSTA combustor investigated using a compressible LES-pdf approach
UR - http://hdl.handle.net/10044/1/84615
ER -