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Adaptive instability suppression controls in a liquid-fueled combustor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kopasakis, George DeLaat, John C. |
| Copyright Year | 2002 |
| Description | An adaptive control algorithm has been developed for the suppression of combustion thermo-acoustic instabilities. This technique involves modulating the fuel flow in the combustor with a control phase that continuously slides within the stable phase region, in a back and forth motion. The control method is referred to as Adaptive Sliding Phasor Averaged Control (ASPAC). The control method is evaluated against a simplified simulation of the combustion instability. Plans are to validate the control approach against a more physics-based model and an actual experimental combustor rig. |
| File Size | 362532 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020084981 |
| Archival Resource Key | ark:/13960/t5k984r41 |
| Language | English |
| Publisher Date | 2002-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Combustion Control Stability Algorithms Simulation Combustion Stability Modulation Sliding Air Breathing Engines Acoustic Instability Fuel Flow Combustion Chambers Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |