supported by the National Key Research and Development Program of China(No.2020YFA0405700).
Quantitative measurement of Soot Volume Fraction (SVF) is an essential prerequisite for controlling soot particle emissions from aero-engine combustors. As an in-situ and non-intrusive optical diagnostic technique, La...
financially supported by the General Program Supported by Educational Committee of Liaoning Province of China(LJKMZ20220537);the financial support from the National Science and Technology Major Project(2017-Ⅲ-0006-0031);the fundamental research funds for the universities of Liaoning Province。
In this study,focusing on the geometry characteristics of spherical expanding flame,the turbulent premixed flames of natural gas/air mixtures were investigated in a fan-stirred turbulent combustor.The effects of initi...
Advanced Jet Propulsion Innovation Center,AEAC(Project ID.HKCX2021-01-021);The Fundamental Research Funds for the Central Universities(Project ID.501XTCX2023146001);Science Center for Gas Turbine Project(P2022-A-II-006-001)。
This paper focuses on the optimization of the outlet temperature field of a hydrogen micromixing diffusion combustor for a micro-turbojet engine with a thrust of 20kgf.The joint simulation optimization platform was es...
supported by the Ministry of Science and Technology of China(Grant No.2022YFE0209000);the Shanghai Rising-Star Program(Grant No.21QB1403900);Shanghai Municipal Commission of Science and Technology(Grant No.22170712600)。
Thermochemical recuperation heat recovery is an advanced waste heat utilization technology that can effectively recover exhaust waste heat from oxy-fuel Stirling engines.The novel combustor of a Stirling engine with t...
The paper sheds light on the idle lean blow off(LBO)problem for high fuel air ratio(FAR)com⁃bustor,which is impossible to be addressed with traditional aero combustor design.A significant improvement in aero combustor...
supported by the National Natural Science Foundation of China (Grant Nos.52276185,52276189 and 51976057);the Fundamental Research Funds for the Central Universities (Grant No.2021MS126);the Natural Science Foundation of Jiangsu Province (Grant No.BK20231209);the Proof-of-Concept Project of Zhongguancun Open Laboratory (Grant No.20220981113)。
Flame temperature and spectral emissivity were the important parameters characterizing the sufficient degree of fuel combustion and the particle radiative characteristics in the Rocket Based Combined Cycle(RBCC)combus...
UK EPSRC funding support through research grant No.EP/M01536X/1.
The choice of a type of combustion technology to be used for heat or power generation depends on economic,technical,operational and fuel availability constraints.The benefits associated with the evolving market driven...
supported by the National Natural Science Foundation of China (Grant No.11972139 and 52125603);the Fundamental Research Funds for the Central Universities (HIT.BRET.2021006 and FRFCU5710094620).
Accurate acquisition of the distribution offlow parameters inside the supersonic combustor is of great significance for hypersonicflight control.It is an interesting attempt to introduce a data-driven model to a super...
Staged combustion of biomass is the most suitable thermo-chemical conversion for achieving lower gaseous emissions and higher fuel conversion rates.In a staged fixed bed combustion of biomass,combustion air is supplie...
supported by the National Science Fund for Distinguished Young Scholars (Grant No. 51825605)。
This paper experimentally studied the effect of CO_(2) opposing multiple jets on the thermoacoustic instability and NO_(x) emissions in a lean-premixed model combustor.The feasibility was verified from three variables...