期刊
JOURNAL OF PROPULSION AND POWER
卷 35, 期 3, 页码 552-564出版社
AMER INST AERONAUTICS ASTRONAUTICS
DOI: 10.2514/1.B37057
关键词
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资金
- U.S. Air Force Office of Scientific Research as part of the National Center for Hypersonic Combined Cycle Propulsion [FA 9550-09-1-0611]
Formaldehyde (CH2O) planar laser- induced fluorescence (PLIF) imaging was performed in a premixed, ethylenefueled dual- mode scramjet combustor to study the flame structure and dynamic flame behavior. CH2OPLIF is used as a marker to provide information on the structure and position of the lower-temperature portion of the reaction zone. Low-repetition-rate (10 Hz) measurements were acquired at several cross-flow planes along the axial flow direction. Statistical analysis of the CH2O topology indicates sparse concentrations of formaldehyde that are intermittently detected by the PLIF measurement. Comparisons between previous large-eddy simulations, laboratory-scale flames, and the current experimental measurements indicate discrepancies between the expected and measured formaldehyde concentrations and structure. High-speed formaldehyde PLIF also was conducted at 50 kHz to further investigate the intermittency of the formaldehyde layers in the flow.
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