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Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement

Aerospace science and technology, 2020-03, Vol.98, p.105594, Article 105594

2020

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Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference

Applied thermal engineering, 2018-02, Vol.130, p.1598-1609

2018

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Performance Assessment of Closed-Brayton-Cycle and Thermoelectric Generator Combined Power Generation System Coupled with Hydrocarbon-Fueled Scramjet

Energies (Basel), 2023-11, Vol.16 (21), p.7385

2023

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Dynamic Characteristics Analysis for a Novel Double-Rotor He-Xe Closed-Brayton-Cycle Space Nuclear Power Generation System

Energies (Basel), 2023-09, Vol.16 (18), p.6620

2023

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All-Dielectric Nanostructured Metasurfaces with Ultrahigh Color Purity and Selectivity for Refractive Index Sensing Applications

Results in physics, 2022-12, Vol.43, p.106092, Article 106092

2022

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Quasi-One-Dimensional Model of Hydrocarbon-Fueled Scramjet Combustor Coupled with Regenerative Cooling

International Journal of Aerospace Engineering, 2022-08, Vol.2022, p.1-14

2022

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Design and Performance of a Compact Air-Breathing Jet Hybrid-Electric Engine Coupled With Solid Oxide Fuel Cells

Frontiers in energy research, 2021-02, Vol.8

2021

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Research progress on active thermal protection for hypersonic vehicles

Progress in aerospace sciences, 2020-11, Vol.119, p.100646, Article 100646

2020

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Performance evaluation of fuel indirect cooling based thermal management system using liquid metal for hydrocarbon-fueled scramjet

Energy (Oxford), 2022-12, Vol.260, p.125068, Article 125068

2022

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A novel liquid metal MHD enhanced Closed-Brayton-Cycle power generation system for hypersonic vehicles: Thermodynamic analysis and performance evaluation with finite cold source

Energy conversion and management, 2022-09, Vol.268, p.116068, Article 116068

2022

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Matching and performance analysis of a solid oxide fuel cell turbine-less hybrid electric propulsion system on aircraft

Energy (Oxford), 2023-01, Vol.263, p.125655, Article 125655

2023

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Performance comparison of three chemical precooled turbine engine cycles using methanol and n-decane as the precooling fuels

Energy (Oxford), 2022-06, Vol.249, p.123606, Article 123606

2022

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Comprehensive technical analyses of a solid oxide fuel cell turbine-less hybrid aircraft propulsion system using ammonia and methane as alternative fuels

Applied thermal engineering, 2023-07, Vol.230, p.120787, Article 120787

2023

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Performance evaluation and off-design strategy of a high temperature proton exchange membrane fuel cell turbine-less hybrid system for low pressure ratio and Mach number aircraft

Journal of power sources, 2023-04, Vol.562, p.232752, Article 232752

2023

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A comprehensive evaluation of ducted fan hybrid engines integrated with fuel cells for sustainable aviation

Renewable & sustainable energy reviews, 2023-10, Vol.185, p.113567, Article 113567

2023

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Performance comparison between closed-Brayton-cycle power generation systems using supercritical carbon dioxide and helium–xenon mixture at ultra-high turbine inlet temperatures on hypersonic vehicles

Energy (Oxford), 2024-04, Vol.293, p.130653, Article 130653

2024

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Performance evaluation for a combined power generation system of closed-Brayton-cycle and thermoelectric generator with finite cold source at room temperature on hypersonic vehicles

Energy (Oxford), 2022-09, Vol.254, p.124444, Article 124444

2022

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Performance comparison of single- and multi-stage onboard thermoelectric generators and stage number optimization at a large temperature difference

Applied thermal engineering, 2018-08, Vol.141, p.456-466

2018

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Influence of water injection on performance of scramjet engine

Energy (Oxford), 2020-06, Vol.201, p.117477, Article 117477

2020

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Evaluation of the CBC-ORC energy system in lunar base: Working fluid combination selection, day and night operation performance

Energy conversion and management, 2022-04, Vol.257, p.115445, Article 115445

2022

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Power optimization and comparison between simple recuperated and recompressing supercritical carbon dioxide Closed-Brayton-Cycle with finite cold source on hypersonic vehicles

Energy (Oxford), 2019-08, Vol.181, p.1189-1201

2019

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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

Applied thermal engineering, 2023-01, Vol.218, p.119303, Article 119303

2023

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Performance analysis of fuel vapor turbine and closed-Brayton-cycle combined power generation system for hypersonic vehicles

Energy (Oxford), 2023-03, Vol.266, p.126426, Article 126426

2023

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Performance analysis of a thermal management system based on hydrocarbon-fuel regenerative cooling technology for scramjets

Energy (Oxford), 2023-12, Vol.285, p.128720, Article 128720

2023

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Performance comparison of liquid metal cooling system and regenerative cooling system in supersonic combustion ramjet engines

Energy (Oxford), 2023-07, Vol.275, p.127488, Article 127488

2023

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Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement

Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference

Performance Assessment of Closed-Brayton-Cycle and Thermoelectric Generator Combined Power Generation System Coupled with Hydrocarbon-Fueled Scramjet

Dynamic Characteristics Analysis for a Novel Double-Rotor He-Xe Closed-Brayton-Cycle Space Nuclear Power Generation System

All-Dielectric Nanostructured Metasurfaces with Ultrahigh Color Purity and Selectivity for Refractive Index Sensing Applications

Quasi-One-Dimensional Model of Hydrocarbon-Fueled Scramjet Combustor Coupled with Regenerative Cooling

Design and Performance of a Compact Air-Breathing Jet Hybrid-Electric Engine Coupled With Solid Oxide Fuel Cells

Research progress on active thermal protection for hypersonic vehicles

Performance evaluation of fuel indirect cooling based thermal management system using liquid metal for hydrocarbon-fueled scramjet

A novel liquid metal MHD enhanced Closed-Brayton-Cycle power generation system for hypersonic vehicles: Thermodynamic analysis and performance evaluation with finite cold source

Matching and performance analysis of a solid oxide fuel cell turbine-less hybrid electric propulsion system on aircraft

Performance comparison of three chemical precooled turbine engine cycles using methanol and n-decane as the precooling fuels

Comprehensive technical analyses of a solid oxide fuel cell turbine-less hybrid aircraft propulsion system using ammonia and methane as alternative fuels

Performance evaluation and off-design strategy of a high temperature proton exchange membrane fuel cell turbine-less hybrid system for low pressure ratio and Mach number aircraft

A comprehensive evaluation of ducted fan hybrid engines integrated with fuel cells for sustainable aviation

Performance comparison between closed-Brayton-cycle power generation systems using supercritical carbon dioxide and helium–xenon mixture at ultra-high turbine inlet temperatures on hypersonic vehicles

Performance evaluation for a combined power generation system of closed-Brayton-cycle and thermoelectric generator with finite cold source at room temperature on hypersonic vehicles

Performance comparison of single- and multi-stage onboard thermoelectric generators and stage number optimization at a large temperature difference

Influence of water injection on performance of scramjet engine

Evaluation of the CBC-ORC energy system in lunar base: Working fluid combination selection, day and night operation performance

Power optimization and comparison between simple recuperated and recompressing supercritical carbon dioxide Closed-Brayton-Cycle with finite cold source on hypersonic vehicles

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

Performance analysis of fuel vapor turbine and closed-Brayton-cycle combined power generation system for hypersonic vehicles

Performance analysis of a thermal management system based on hydrocarbon-fuel regenerative cooling technology for scramjets

Performance comparison of liquid metal cooling system and regenerative cooling system in supersonic combustion ramjet engines

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