Associate Professor
Telephone：027-87540185
E-mail：luofeiteng@hust.edu.cn
Academic Areas：Flight Vehicle Design and Aerospace Propulsion
Research Interests：Hypersonic Aircraft; Hypersonic Propulsion including Ramjet, Scramjet and Combined Cycle Engine; Flow and Combustion for Propulsion
Academic Degrees
PhD in Aerospace Propulsion Theory and Engineering, 2012, Northwestern Polytechnical University, China
Bachelor in Flight Vehicle Design and Engineering, 2006, Northwestern Polytechnical University, China
Professional Experience
2018-present：Associate Professor, School of Aerospace Engineering, Huazhong University of Science and Technology.
2012-2018：Senior Engineer, Science and Technology on Scramjet Lab, The Third Research Institute of China Aerospace Science and Industry Corporation Limited (CASIC).
Selected Publications
[1] Feiteng LUO，Wenyan SONG，Zhiqiang ZHANG，Weiqiang LI，Jianping LI. Experimental and Numerical Studies of Vitiated Air Effects on Hydrogen-fueled Supersonic Combustor Performance[J]. Chinese Journal of Aeronautics, Vol.25（2）, April 2012, P164-172.（SCI）
[2] Jianping Li, Wenyan Song, Feiteng Luo, Deyong Shi. Experimental investigation of vitiation effects on supersonic combustor performance[J]. Acta Astronautica, Vol.96, March–April 2014, P296-302.（SCI）
[3] Li Jianping, Song Wenyan, Xing Ying, Luo Feiteng. Influences of Geometric Parameters upon Nozzle Performances in Scramjets[J]. Chinese Journal of Aeronautics, Vol.21（6）, December 2008, P506-511.（SCI）
[4] LUO Feiteng, GANG Qiang, MA Jun, LING Wenhui. Preliminary Design and Performance Studies of a Wide Range Rocket-based Combined Cycle Engine[C]. 67th International Astronautical Congress (IAC2016)，Guadalajara, Mexico (26-30 Sept. 2016).（EI）
[5] LUO Feiteng, FENG Shuo, TIAN Yufei，GANG Qiang. Analysis of Thermal Throat Characteristics of a Wide-Range RBCC Combustor at Ramjet Mode[C]. Asian Joint Conference on Propulsion and Power (AJCPP), Xiamen, CHINA (14–17 March 2018).
[6] Qu Jianxiong, Luo Feiteng, Tian Yufei. Primary/Secondary Flow Mixing Characteristics in the RBCC Flowpath[C]. AIAA International Space Planes and Hypersonics Technologies Conference. 2017.（EI）
[7] Wei Qiang Li, Fei Teng Luo. Investigation of Performance of Scramjet Combustion Used Kerosene with Clean Air[J]. Advanced Materials Research, Vol. 601, pp. 294-298, 2013.（EI）
[8] Wei Baoxi, Ling Wenhui, Luo Feiteng, Gang Qiang. Propulsion Performance Research and status of TRRE Engine experiment[C]. AIAA International Space Planes and Hypersonics Technologies Conference. 2017.（EI）
[9] Luo Chunqin，Wei Baoxi，Luo Feiteng. Design and experimental investigation of RBCC engine operating from Mach 2.0 to 6.0[C]. 65th International Astronautical Congress (IAC 2014)，Toronto, Canada，2014.9.29-2014.10.3.（EI）
[10] LUO Fei-teng , SONG Wen-yan, LIU Wei-xiong , LI Jian-ping. Investigation of cored bricks matrix preliminary design and thermal analysis for high temperature wind tunnel storage heater[J]. Journal of Experiments in Fluid Mechanics, Vol.1:38-45, 2013.（in Chinese, EI）
[11] LUO Feiteng，SONG Wenyan，LIU Hao. Experimental investigation for vitiated air effects on hydrogen-fueled supersonic combustor performance[J]. Journal of Propulsion Technology，2010，31（4）：401-405.（in Chinese, EI）
[12] LUO Feiteng，SONG Wenyan，LI Jianping, LI Qiang. Research on turbofan engine HP-compressor rotor-12 blade tip clearance control[J]. Journal of Aerospace Power，2009，24（4）：851-858.（in Chinese, EI）
Courses Taught
AE2051 Jet and rocket engine：for undergraduate, 48 hours per semester.
Project
Vitiation effects on supersonic combustion characteristics
High temperature clean air direct-connected experimental system design
Thermal throat adjustment of a Wide-Range RBCC
Primary-Secondary flow Interaction processes and characteristics in RBCC flowpath
Awards
