Special Session 8

 

Aerospace Combustion Engineering | 空天发动机燃烧


Introducation:

Combustion still plays a fundamental role in all the applications requiring high energy density. Thermo-chemical systems, even in the future, will continue to dominate the field of rocketry and of long-range aero-engines. The need for a cleaner thrust production for aerospace systems cannot be achieved regardless of a deeper understanding of the fundamentals involved in combustion and its applications. Combustion for aerospace engineering should be further investigated in order to increase the efficiency of the utilization of the energy released and to decrease its impact through CO2 and other pollutant emissions. This Special Issue offers the opportunity to publish cutting edge research and investigations on fundamentals and applications of combustion, on novel techniques and instrumentations to monitor and diagnose flow characteristics within flames and expanding gases, on new types of fuels and propellants that require improved combustors or burners, on the development of improved modelling and simulation techniques of the processes involved in combustion, including heat transfer, flame dynamics, turbulence, mixing, chemical reactions, and equilibrium. Submissions are welcomed in the field of solid, liquid and hybrid rockets, gas turbines, internal combustion engines, aerospikes, ramjets, scramjets, as well as fundamental combustion studies with particular interest in work relating to aerospace applications.

 

Organizers:

Qingfei Fu, Beihang University, China

Qingfei Fu is a Professor at the School of Astronautics, Beihang University, and a Changjiang Scholar Distinguished Professor. He currently serves as Deputy Director of the Engine Thermal Process Research Center at the National Key Laboratory of Aerospace Liquid Propulsion Technology. In recent years, he has led over 30 research projects, including those funded by the National Natural Science Foundation of China. He was awarded the National Science Fund for Excellent Young Scholars in 2019 and received the Second Prize of the National Technology Invention Award in 2017, along with two provincial/ministerial-level First Prizes for Technology Invention and the ILASS "Hiroshi Hiroyasu Award."

 

Chenglong Tang, Xi’an Jiaotong University, China

Dr. Tang obtained his ph D degree in Xi’an Jiaotong University in 2011. He has been working as a research collaborator in Princeton University from 2009 to 2011. He is now a professor in Xi’an Jiaotong University working on new concept propulsion and reactive flows in liquid rocket engines. His research has received 5 National Natural Science Foundation grants support. Dr. Tang has served as program chair of National Youth Combustion Conference in China. He is now an editorial member in Atomization and Sprays. He is also a Member of Technical Committee, Chinese National Space Science and Technology Center. He won the National Natural Science Award. He is the author/co-author of more than 100 publications in peer reviewed journals, with an H index of 45 in J Fluid Mech, Physics Fluids, Combust Flame, Proc Combust Inst, etc.

 

Submission Guideline:

Please submit your manuscript via Online Submission System: https://easychair.org/my/conference?conf=meae2025
Please choose Special Session: Aerospace Combustion Engineering

 

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