Control of reaction and thermo-acoustic instabilities of a combustion chamber

Simple item page
dc.contributor.authorDebbah, A.
dc.contributor.authorKerboua, A.
dc.contributor.authorKlaiaia, R.
dc.date.accessioned2025-04-21T16:25:43Z
dc.date.available2025-04-21T16:25:43Z
dc.date.issued2021
dc.description.abstractThis paper deals with the improvement of the control and the vanishing of the thermo-acoustic instability in gas-turbine engine combustors via a design of an active controller. The proposed design used a multi-objective genetic algorithm (MOGA) and multi-objective particle swarm optimization (MOPSO) to stabilize the unstable system from limit cycle with uncertain model. These parameters were chosen to minimize four objective functions: the mass fraction of the fuel produced, temperature control, flame fluctuation and the variation in the flow mass rate of input fuel. In addition, an improvement in suppression of the instability was achieved by coupling the combustor and the unsteady heat perturbations and thermos-acoustic models in simulation.
dc.identifier.urihttp://dspace.univ-oeb.dz:4000/handle/123456789/21950
dc.language.isoen
dc.publisherUniversity of Oum El Bouaghi
dc.subjectCombustion instabilities; Thermo-acoustic instability; Active control; Multi-objective optimization
dc.titleControl of reaction and thermo-acoustic instabilities of a combustion chamber
dc.typeArticle
Files
Original bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
Control of reaction and thermo-acoustic instabilities of a.pdf
Size:
487.42 KB
Format:
Adobe Portable Document Format
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed upon to submission
Description:
Download
Collections
The 1 ST international conference on electronics, artificial intelligence and technologies ICEAINT 2021