项目编号: | 1510222
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项目名称: | UNS: Collaborative Research: Turbulent Flame Structure of Cavity Stabilized Reacting Shear Layers: Effects of Flow Compressibility, Heat Release, and Finite-rate Kinetics |
作者: | Jack Edwards
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承担单位: | North Carolina State University
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批准年: | 2014
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开始日期: | 2015-06-01
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结束日期: | 2018-05-31
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资助金额: | USD174000
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资助来源: | US-NSF
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项目类别: | Continuing grant
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国家: | US
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语种: | 英语
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特色学科分类: | Engineering - Chemical, Bioengineering, Environmental, and Transport Systems
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英文关键词: | high-speed
; research
; flow
; understanding flame structure
; research team
; flame stabilization mechanism
; shear flow
; flame structure
; flow geometry
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英文摘要: | 1511791(Chelliah)/1511520(Cutler)/1510222(Edwards)
High-speed and supersonic combustion is of vital importance to high-speed transport. The research team comprised of experimentalist and numerical modelers will try to understand, using a unique facility and state-of-art numerical models, how fuel burning at such high speed happens and how stable combustion can be achieved. A team of undergraduate and graduate students will be involved in the research and the data and results will be widely published.
To understand the flame stabilization mechanism requires the understanding flame structure resulting from the interaction between the chemical reaction, which releases heat, and the flow. Under high-speed conditions, the flow is turbulent. The proposal focuses on this interaction under supersonic conditions where compressibility also plays a role. The flow geometry chosen is high-speed reacting shear flow over cavity, which is commonly believed to be a good candidate for supersonic combustion and propulsion. The proposed facility (located at the lead PI's institution - UVa) is unique, which has been developed over the past decades and is well and appropriately leveraged for the proposed research. Fundamental data on flame structure and statistics on key species are to be obtained experimentally. Computational results using DNS (Direct Numerical Simulation) will supplement the experiments to provide additional information not accessible from experiments in developing submodels, which can be used in the future development of high-speed propulsion combustors. The experimental data are of archival value. Close collaboration proposed with researchers from government labs would likely amplify its usefulness. |
资源类型: | 项目
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标识符: | http://119.78.100.158/handle/2HF3EXSE/94579
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Appears in Collections: | 影响、适应和脆弱性 气候减缓与适应
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Recommended Citation: |
Jack Edwards. UNS: Collaborative Research: Turbulent Flame Structure of Cavity Stabilized Reacting Shear Layers: Effects of Flow Compressibility, Heat Release, and Finite-rate Kinetics. 2014-01-01.
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