Resumen
Next generation combustor technology for gas turbine engines may include lean premixed mixtures injected into high temperature vitiated products such that autoignition can become a potential stabilization mechanism. Fundamental understanding of when autoignition occurs in these complex flowfields is crucial to model future combustors. A simplified flowfield of a premixed jet in vitiated coflow was used in this work to understand how mixing between the two flows can stabilize a steady, laminar autoignition stabilized flame. Chemical simulations in conjunction with both formaldehyde and hydroxyl planar laser induced florescence measurements were performed to identify trends between different cases which influence the stabilization point. Simulations suggest that autoignition should occur much faster than the experimentally observed flow timescale to the stabilization point. Trends between simulation concentrations and experimental fluorescence signals show similarities, but at different timescales. Experiments show that the formaldehyde layer width, which can be thought of as marking the radical pool width, does not correlate to changes in the stability point. Peak formaldehyde signals at the stability point were less than 5% different across all cases examined, indicating that a critical concentration of formaldehyde and radicals formed prior to the flame is necessary to sustain the flame base. However, the flow time to reach the peak levels is inconsistent with the chemical simulation time scales. Therefore, it is proposed that the mixture fraction gradient significantly delays the ignition time.
| Idioma original | English |
|---|---|
| Título de la publicación alojada | AIAA Aerospace Sciences Meeting |
| DOI | |
| Estado | Published - 2018 |
| Evento | AIAA Aerospace Sciences Meeting, 2018 - Kissimmee, United States Duración: ene 8 2018 → ene 12 2018 |
Serie de la publicación
| Nombre | AIAA Aerospace Sciences Meeting, 2018 |
|---|
Conference
| Conference | AIAA Aerospace Sciences Meeting, 2018 |
|---|---|
| País/Territorio | United States |
| Ciudad | Kissimmee |
| Período | 1/8/18 → 1/12/18 |
Nota bibliográfica
Publisher Copyright:© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Financiación
This research is supported by the Kentucky Science and Engineering Foundation under Grant # KSEF-148-502-
| Financiadores | Número del financiador |
|---|---|
| Kentucky Science and Engineering Foundation | KSEF-148-502- |
ASJC Scopus subject areas
- Aerospace Engineering
Huella
Profundice en los temas de investigación de 'Autoignition stabilization of a premixed jet in vitiated coflow'. En conjunto forman una huella única.Citar esto
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