Experimental investigation of limit-cycle oscillations in an unstable gas turbine combustor

Journal of Propulsion and Power

Volumn 18, Issue 1, 2002, Pages 61-67

  Lieuwen, Tim C ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; GAS TURBINES; INTAKE SYSTEMS; OPTIMIZATION; OSCILLATIONS;

GAS TURBINE COMBUSTOR SIMULATORS;

COMBUSTORS;

EID: 0036152849     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5898     Document Type: Article

References (18)

1. Experimental investigation of near-blowout instabilities in a lean, premixed combustor
2. An experimental investigation of combustion dynamics of a lean, premixed swirl injector
3. The role of equivalence ratio oscillations in driving combustion instabilities in low NOx gas turbines
4. Experimental investigation of combustion instabilities in a gas turbine combustor simulator
5. Nonlinear analysis and modeling of combustion instabilities in a laboratory combustor
6. Evidence of a strange attractor in ramjet combustion
7. Phase drift characteristics of self excited, combustion driven oscillations
8. System identification for models of lean premix combustion instability
9. Combustion noise and combustion instabilities in propulsion systems
10. Nonlinear self excited oscillations of a ducted flame
11. Sound absorption by a screen with a regular array of slits
12. Pulsed instabilities in solid-propellant rockets