Zhiyong Lin - Concepedia

Concepedia

Author

Zhiyong Lin

National University of Defense Technology ORCID

Also Known As

Lin Zhi-yong, Zhi-Yong Lin, Zhi-yong Lin, Zhiyong Lin

51

Publications

1.4K

Citations

24

H-Index

34

Concepts

All Affiliations

National University of Defense Technology Space Engineering University Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)University of Southampton

ZL

About

Zhiyong Lin is an author at National University of Defense Technology specializing in engineering, space engineering, and propulsion.

Top Concepts

#	Concept	H-Index	Publications	Citations
1	Engineering	23	26	1.1K
2	Mechanical Engineering	8	8	313
3	Physics	5	5	143
4	Applied Physics	2	2	32
5	Mechanics	2	2	58

Zhiyong Lin

×

31

Publications

1.4K

Citations

24

H-Index

	Year	Citations
An experimental study on CH4/O2 continuously rotating detonation wave in a hollow combustion chamber Wei Lin, Jin Zhou, Shijie Liu, Experimental Thermal and Fluid Science Detonation PhenomenonDetonation WaveCombustion ScienceHollow Combustion ChamberCombustion Engineering	2014	154
Experimental study on propagation mode of H 2 /Air continuously rotating detonation wave Wei Lin, Jin Zhou, Shijie Liu, International Journal of Hydrogen Energy EngineeringDetonation PhenomenonDetonation WaveAerospace EngineeringPropagation Mode	2014	120
Experimental investigation on detonation combustion patterns of hydrogen/vitiated air within annular combustor Chao Wang, Weidong Liu, Shijie Liu, Experimental Thermal and Fluid Science Annular CombustorEngineeringExperimental InvestigationDetonation PhenomenonDetonation Combustion Patterns	2015	95
Experimental verification of air-breathing continuous rotating detonation fueled by hydrogen Chao Wang, Weidong Liu, Shijie Liu, International Journal of Hydrogen Energy Experimental VerificationEngineeringDetonation PhenomenonAerospace EngineeringCombustion Science	2015	84
Numerical investigation of a rotating detonation engine under premixed/non-premixed conditions Jian Sun, Jin Zhou, Shijie Liu, Acta Astronautica AeroacousticsEngineeringDetonation PhenomenonMechanical EngineeringGas Turbine Combustion	2018	82
Effects of injection nozzle exit width on rotating detonation engine Jian Sun, Jin Zhou, Shijie Liu, Acta Astronautica Detonation PhenomenonEngineeringFuel InjectionIn-cylinder FlowPropulsion	2017	67
Effects of air injection throat width on a non-premixed rotating detonation engine Jian Sun, Jin Zhou, Shijie Liu, Acta Astronautica EngineeringDetonation PhenomenonAerospace EngineeringIn-cylinder FlowAerodynamics	2019	54
Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model Xiaodong Cai, Jianhan Liang, Ralf Deiterding, International Journal of Hydrogen Energy AeroacousticsDetailed Reaction ModelEngineeringDetonation PhenomenonAerospace Engineering	2015	53
Numerical investigation of a non-premixed hollow rotating detonation engine Jian Sun, Jin Zhou, Shijie Liu, International Journal of Hydrogen Energy EngineeringDetonation PhenomenonMechanical EngineeringIn-cylinder FlowPropulsion	2019	52
Plume flowfield and propulsive performance analysis of a rotating detonation engine Jian Sun, Jin Zhou, Shijie Liu, Aerospace Science and Technology EngineeringDetonation PhenomenonAerospace EngineeringRocket EngineIn-cylinder Flow	2018	48

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