Song Chen
Song Chen
Research Scientist at the Centre for Climate Research Singapore (CCRS)
Verified email at nea.gov.sg
Title
Cited by
Cited by
Year
RANS investigation of the effect of pulsed fuel injection on scramjet HyShot II engine
S Chen, D Zhao
Aerospace Science and Technology 84, 182-192, 2019
402019
Numerical study of non-reacting flowfields of a swirling trapped vortex ramjet combustor
S Chen, D Zhao
Aerospace Science and Technology 74, 81-92, 2018
192018
Numerical study of dynamic response of a jet diffusion flame to standing waves in a longitudinal tube
S Chen, D Zhao, HKH Li, TY Ng, X Jin
Applied Thermal Engineering 112, 1070-1082, 2017
172017
Numerical Investigation of a Trapped Vortex Miniature Ramjet Combustor
Song Chen, Randy S. M. Chue, Jörg Schlüter, Tue T. Q. Nguyen, and Simon C. M. Yu
Journal of Propulsion and Power 31 (3), 872-882, 2015
142015
High-temperature effects on aerodynamic and acoustic characteristics of a rectangular supersonic jet
S Chen, R Gojon, M Mihaescu
2018 AIAA/CEAS aeroacoustics conference, 3303, 2018
122018
Spinning Effects on a Trapped Vortex Combustor
S Chen, RSM Chue, SCM Yu, JU Schlüter
Journal of Propulsion and Power 32 (5), 1133-1145, 2016
122016
Numerical study of guide vane effects on reacting flow characteristics in a trapped vortex combustor
S Chen, D Zhao
Combustion Science and Technology 190 (12), 2111-2133, 2018
112018
Nozzle pressure ratio effects on aerodynamics and acoustics of a highly-heated rectangular supersonic jet
S Chen, M Mihaescu
25th AIAA/CEAS Aeroacoustics Conference, 2753, 2019
52019
Numerical study of a methane jet diffusion flame in a longitudinal tube with a standing wave
S Chen, H Zhao, KJ Tay, AA Tarique
Energy Procedia 105, 1539-1544, 2017
42017
Numerical Investigations of Small-Size High Throughflow Speed Combustors with Trapped-Vortex Concept
S Chen, RSM Chue, TTQ Nguyen, SCM Yu
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2013
32013
Numerical study of Dynamic Response of different Fuels Jet Diffusion Flame to standing waves in a Longitudinal Tube
X Jin, S Chen, S Li, H Zhao
Energy Procedia 105, 4842-4847, 2017
22017
Numerical study of trapped vortex combustors characteristics in small Ramjets
S Chen
PhD Thesis, 2016
22016
Numerical Investigation of Pulsed Fuel Injections for the HyShot II
S Chen, D Zhao
21st AIAA International Space Planes and Hypersonics Technologies Conference …, 2017
12017
Effects of Strong Spinning Motion on Trapped Vortex Combustors
S Chen, RSM Chue, JU Schlüter, SCM Yu
AIAA 2015-3299, 2015
1*2015
Flow and aeroacoustic attributes of highly-heated transitional rectangular supersonic jets
S Chen, R Gojon, M Mihaescu
Aerospace Science and Technology, 106747, 2021
2021
Effect of an Adjacent Flat Plate on a Highly-Heated Rectangular Supersonic Jet
S Chen, R Gojon, M Mihaescu
AIAA Scitech 2020 Forum, 0746, 2020
2020
Effects of Spinning Motion on the Flowfield Characteristics of Trapped Vortex Combustors
S Chen, RSM Chue, J Schluter, S Yu
AIAA Aviation Forum: 33rd AIAA Applied Aerodynamics Conference, 2015
2015
Design Studies of a Small-Size Subsonic Trapped Vortex Combustor
RSM Chue, S Chen, TTQ Nguyen
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