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Kunlin Cheng

ORCID: 0009-0007-3140-8972
Observed ORCIDs: 0009-0007-3140-8972, 0000-0002-3556-934X
OpenAlex ID: A5084656953
Research progress on active thermal protection for hypersonic vehicles
2020 · Silong Zhang, Xin Li, et al. · Progress in Aerospace Sciences · 432
Power optimization and comparison between simple recuperated and recompressing supercritical carbon dioxide Closed-Brayton-Cycle with finite cold source on hypersonic vehicles
2019 · Kunlin Cheng, Jiang Qin, et al. · Energy · 100
Quasi-One-Dimensional Model of Scramjet Combustor Coupled with Regenerative Cooling
2016 · Duo Zhang, Yu Feng, et al. · Journal of Propulsion and Power · 97
Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement
2019 · Youyin Wang, Kunlin Cheng, et al. · Aerospace Science and Technology · 83
Thermodynamic analysis of a solid oxide fuel cell jet hybrid engine for long-endurance unmanned air vehicles
2019 · Zhixing Ji, Jiang Qin, et al. · Energy Conversion and Management · 82
Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference
2017 · Kunlin Cheng, Jiang Qin, et al. · Applied Thermal Engineering · 69
Experimental and theoretical investigation of power generation scheme driven by thermal cracked gaseous hydrocarbon fuel for hypersonic vehicle
2018 · Haowei Li, Jiang Qin, et al. · Energy Conversion and Management · 68
Performance assessment of a closed-recuperative-Brayton-cycle based integrated system for power generation and engine cooling of hypersonic vehicle
2019 · Kunlin Cheng, Jiang Qin, et al. · Aerospace Science and Technology · 66
Performance comparison of single- and multi-stage onboard thermoelectric generators and stage number optimization at a large temperature difference
2018 · Kunlin Cheng, Jiang Qin, et al. · Applied Thermal Engineering · 54
Performance analysis of fuel vapor turbine and closed-Brayton-cycle combined power generation system for hypersonic vehicles
2022 · Chaolei Dang, Kunlin Cheng, et al. · Energy · 51
Performance evaluation of a turbojet engine integrated with interstage turbine burner and solid oxide fuel cell
2018 · Zhixing Ji, Jiang Qin, et al. · Energy · 51
Thermodynamic analysis for high-power electricity generation systems based on closed-Brayton-cycle with finite cold source on hypersonic vehicles
2018 · Kunlin Cheng, Jiang Qin, et al. · International Journal of Hydrogen Energy · 49
Evaluation of the CBC-ORC energy system in lunar base: Working fluid combination selection, day and night operation performance
2022 · Zekuan Liu, Kunlin Cheng, et al. · Energy Conversion and Management · 47
Performance Evaluation of Fuel Indirect Cooling Based Thermal Management System Using Liquid Metal for Hydrocarbon-Fueled Scramjet
2022 · Kunlin Cheng, Jing Xu, et al. · Energy · 46
Performance analysis of a turbofan engine integrated with solid oxide fuel cells based on Al-H2O hydrogen production for more electric long-endurance UAVs
2021 · Fafu Guo, Jiang Qin, et al. · Energy Conversion and Management · 46
Performance analysis of a thermal management system based on hydrocarbon-fuel regenerative cooling technology for scramjets
2023 · Chaolei Dang, Kunlin Cheng, et al. · Energy · 44
Performance analysis of the heat pipe-based thermoelectric generator (HP-TEG) energy system using in-situ resource for heat storage applied to the early-period lunar base
2022 · Zekuan Liu, Kunlin Cheng, et al. · Applied Thermal Engineering · 44
Thermodynamic performance evaluation of a turbine-less jet engine integrated with solid oxide fuel cells for unmanned aerial vehicles
2019 · Zhixing Ji, Jiang Qin, et al. · Applied Thermal Engineering · 44
A novel liquid metal MHD enhanced Closed-Brayton-Cycle power generation system for hypersonic vehicles: Thermodynamic analysis and performance evaluation with finite cold source
2022 · Kunlin Cheng, Yilin Wang, et al. · Energy Conversion and Management · 42
Performance comparison of liquid metal cooling system and regenerative cooling system in supersonic combustion ramjet engines
2023 · Jing Xu, Kunlin Cheng, et al. · Energy · 39
Comparative performance analysis of solid oxide fuel cell turbine-less jet engines for electric propulsion airplanes: Application of alternative fuel
2019 · Zhixing Ji, Jiang Qin, et al. · Aerospace Science and Technology · 39
Thermodynamics analysis of a turbojet engine integrated with a fuel cell and steam injection for high-speed flight
2019 · Zhixing Ji, Jiang Qin, et al. · Energy · 39
Performance assessment of closed Brayton cycle-organic Rankine cycle lunar base energy system: Thermodynamic analysis, multi-objective optimization
2023 · Zekuan Liu, Zixuan Wang, et al. · Energy · 38
Comprehensive technical analyses of a solid oxide fuel cell turbine-less hybrid aircraft propulsion system using ammonia and methane as alternative fuels
2023 · Fafu Guo, Chengjie Li, et al. · Applied Thermal Engineering · 38
Performance assessment of an integrated power generation and refrigeration system on hypersonic vehicles
2019 · Kunlin Cheng, Jiang Qin, et al. · Aerospace Science and Technology · 37
Works count: 91
Citation count: 2,610
H-index: 31
I10-index: 64
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