Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor

	Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor
	Yao W(姚卫); Li B(李波)
会议录名称	AIAA Propulsion and Energy Forum and Exposition, 2019
	2019
会议名称	AIAA Propulsion and Energy Forum and Exposition, 2019
会议日期	August 19, 2019 - August 22, 2019
会议地点	Indianapolis, IN, United states
摘要	A dynamic zone flamelet model is proposed and validated in this study. The model divides the whole computational domain into different zones and uses a local flamelet to describe the chemistry status within each zone. The zone division constantly updates with the time-variant mixture fraction fields. Each zone is in irregular shape and contains a random number of CFD cells. The flamelet evolution equation due to convective transport, molecular diffusion, and chemical reactions is derived through redefining the conditional average within each zone. In highly compressible supersonic flows, the density, temperature, and velocity do not correlate with the mixture fraction any more; thus only the species mass fraction in each flamelet is used. The flamelet temperature equation is not solved, but a computationally-efficient statistical method is used for the conditional temperature, which then determines the reaction progress. The DZFM is then applied to a GH2/GO2 rocket combustor based on an Improved Delayed Detached Eddy Simulation (IDDES) framework and a total of 20,557 flamelet zones. The predicted wall heat flux, mean temperature and mean hydrogen concentration are generally comparable with the available experimental measurement and the previous predictions in the literature. The evolution of flamelet variables with the axial height and the time shows that the current model has the capability of characterizing the transient chemistry status, which would especially useful for unsteady combustion modeling by large eddy simulation. © 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
关键词	Dynamic zone flamelet model GH2/GO2 Large Eddy Simulation (LES) Rocket combustor Turbulence-chemistry interaction
ISBN号	9781624105906
URL	查看原文
收录类别	EI
语种	英语
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/85099
专题	高温气体动力学国家重点实验室
作者单位	1.Key Laboratory of High-Temperature Gas Dynamics, Institute of Mechanics, CAS, Beijing, 100190, China 2.School of Engineering Science, University of Chinese Academy of Science, Beijing, 100049, China
推荐引用方式 GB/T 7714	Yao W,Li B. Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor[C]AIAA Propulsion and Energy Forum and Exposition, 2019,2019.

条目包含的文件		下载所有文件
文件名称/大小	文献类型	版本类型	开放类型	使用许可
CpA2019013.pdf（1665KB）	会议论文		开放获取	CC BY-NC-SA	浏览下载