Segui
Can Ruan (阮灿)
Can Ruan (阮灿)
Email verificata su forbrf.lth.se
Titolo
Citata da
Citata da
Anno
Flameless combustion with liquid fuel: A review focusing on fundamentals and gas turbine application
F Xing, A Kumar, Y Huang, S Chan, C Ruan, S Gu, X Fan
Applied Energy 193, 28-51, 2017
1482017
Experimental and kinetic modeling study of ignition characteristics of RP-3 kerosene over low-to-high temperature ranges in a heated rapid compression machine and a heated …
Y Mao, L Yu, Z Wu, W Tao, S Wang, C Ruan, L Zhu, X Lu
Combustion and Flame 203, 157-169, 2019
1042019
Principles of non-intrusive diagnostic techniques and their applications for fundamental studies of combustion instabilities in gas turbine combustors: A brief review
C Ruan, F Chen, W Cai, Y Qian, L Yu, X Lu
Aerospace Science and Technology 84, 585-603, 2019
1022019
Effects of fuel variation and inlet air temperature on combustion stability in a gas turbine model combustor
F Chen, C Ruan, T Yu, W Cai, Y Mao, X Lu
Aerospace Science and Technology 92, 126-138, 2019
652019
Time-resolved measurements of a swirl flame at 4 kHz via computed tomography of chemiluminescence
T Yu, C Ruan, H Liu, W Cai, X Lu
Applied Optics 57 (21), 5962-5969, 2018
412018
Investigation of engine performance for alcohol/kerosene blends as in spark-ignition aviation piston engine
G Liu, C Ruan, Z Li, G Huang, Q Zhou, Y Qian, X Lu
Applied energy 268, 114959, 2020
392020
Numerical investigation on shock train control and applications in a scramjet engine
F Xing, C Ruan, Y Huang, X Fang, Y Yao
Aerospace Science and Technology 60, 162-171, 2017
392017
Experimental study on flame/flow dynamics in a multi-nozzle gas turbine model combustor under thermo-acoustically unstable condition with different swirler configurations
C Ruan, F Chen, T Yu, W Cai, X Li, X Lu
Aerospace Science and Technology 98, 105692, 2020
382020
A study on the low-to-intermediate temperature ignition delays of long chain branched paraffin: Iso-cetane
L Yu, Y Qiu, Y Mao, S Wang, C Ruan, W Tao, Y Qian, X Lu
Proceedings of the Combustion Institute 37 (1), 631-638, 2019
372019
An experimental and kinetic modeling study of n-butylcyclohexane over low-to-high temperature ranges
Y Mao, S Wang, Z Wu, Y Qiu, L Yu, C Ruan, F Chen, L Zhu, X Lu
Combustion and Flame 206, 83-97, 2019
352019
Experimental characterization of the spatiotemporal dynamics of a turbulent flame in a gas turbine model combustor using computed tomography of chemiluminescence
C Ruan, T Yu, F Chen, S Wang, W Cai, X Lu
Energy 170, 744-751, 2019
352019
Experimental study on combustion stability characteristics in liquid-fueled gas turbine model combustor: Fuel sensitivities and flame/flow dynamics
C Ruan, F Chen, T Yu, W Cai, Y Mao, Y Qian, X Li, X Lu
Fuel 265, 116973, 2020
252020
Measurement of the 3D Rayleigh index field via time-resolved CH* computed tomography
T Yu, C Ruan, F Chen, Q Wang, W Cai, X Lu
Aerospace Science and Technology 95, 105487, 2019
212019
An experimental and kinetic modeling study of a four-component surrogate fuel for RP-3 kerosene
Y Mao, J Xia, C Ruan, Z Wu, Y Feng, J Zhu, S Wang, L Yu, X Lu
Proceedings of the Combustion Institute 38 (1), 555-563, 2021
182021
Development of an absorption-corrected method for 3D computed tomography of chemiluminescence
T Yu, Z Li, C Ruan, F Chen, X Lu, W Cai
Measurement Science and Technology 30 (4), 045403, 2019
182019
A parametrical study of the breakup and atomization process of two impinging liquid jets
C Ruan, F Xing, Y Huang, L Xu, X Lu
Atomization and sprays 27 (12), 2017
172017
Study of the dump diffuser optimization for gas turbine combustors
L Xu, Y Huang, C Ruan, PWF Xing
Procedia engineering 99, 828-834, 2015
162015
A quantitative evaluation method of 3D flame curvature from reconstructed flame structure
T Yu, Q Wang, C Ruan, F Chen, W Cai, X Lu, M Klein
Experiments in Fluids 61, 1-13, 2020
152020
The brief introduction of different laser diagnostics methods used in aeroengine combustion research
F Xing, Y Huang, M Zhao, J Zhao
Journal of Sensors 2016 (1), 2183569, 2016
152016
Experimental characterization of flame/flow dynamics during transition between stable and thermo-acoustically unstable conditions in a gas turbine model combustor
C Ruan, F Chen, T Yu, W Cai, X Li, X Lu
Aerospace Science and Technology 102, 105858, 2020
142020
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