High Frequency Transverse Acoustic Coupling in a Multiple Injector Cryogenic Combustor - Archive ouverte HAL Accéder directement au contenu
Article Dans Une Revue Journal of Propulsion and Power Année : 2006

High Frequency Transverse Acoustic Coupling in a Multiple Injector Cryogenic Combustor

Résumé

High-frequency combustion oscillations are investigated experimentally. The combustor fed by cryogenic propellants operates under elevated pressure conditions (pc = 0.9 MPa) and is equipped with three coaxial injectors fed by liquid oxygen and gaseous methane. Injection parameters are in the typical range used in rocket engines. This experiment simulates on a model scale conditions prevailing in such systems, but full similarity is not achieved. The chamber exhibits a set of resonant modes with eigenfrequencies above 1 kHz. The study focuses on high-frequency dynamics resulting from a strong coupling between one of the transverse modes and combustion. The combustor is forced with an external actuator. The eigenmodes are identified with a linear frequency sweep, and then the system is modulated at the first transverse resonant frequency. The flame motion and response are observed with a high speed and two intensified charge-coupled-device cameras recording phase-conditioned images. In a set of experiments carried out on the multiple-injector combustor, operating conditions were changed systematically to determine parameter ranges leading to combustion sensitivity to transverse excitation. Strong coupling is observed in this way with a spectacular modification of the flame spread. Emission from the three flames is notably intensified when this coupling occurs, whereas thermocouples placed on the lateral walls detect a rapid increase in temperature. The OH∗ emission intensity that can be linked to the heat-release rate is increased. A phase analysis indicates that the pressure and OH∗ emission oscillate transversally and in phase at the modulation frequency. This behavior is also observed with the high-speed camera, which also features enhanced reactive vortices convected in the downstream direction at a lower frequency.
Fichier non déposé

Dates et versions

hal-00184034 , version 1 (30-10-2007)

Identifiants

Citer

Franck Richecoeur, Philippe Scouflaire, Sébastien Ducruix, Sébastien M. Candel. High Frequency Transverse Acoustic Coupling in a Multiple Injector Cryogenic Combustor. Journal of Propulsion and Power, 2006, 22 (4), pp.790-799. ⟨10.2514/1.18539⟩. ⟨hal-00184034⟩
104 Consultations
0 Téléchargements

Altmetric

Partager

Gmail Facebook X LinkedIn More