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Yakun Huang

Nanjing University of Science and Technology

H指数:14

被引数:534

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Ignition and blowout of spray flame evolution of an evaporative flameholder under uniform subsonic and subsonic-supersonic inflows

在均匀亚声速和亚声速-超声速进气条件下的蒸发式火焰稳定器喷雾火焰的点火与熄火演化

Aerospace Science and Technology

IF5.8

2026-02-220

PRE

Combustion performance of an evaporative flameholder under subsonic-supersonic mixing inflow

APPLIED THERMAL ENGINEERING

IF6.9

2025-01-010

PRE

Flame evolution characteristics during ignition of a combined flameholder fueled by RP-3 liquid kerosene

APPLIED THERMAL ENGINEERING

IF6.9

2024-11-010

PRE

Comparison of fluid structure downstream of an evaporative flameholder with subsonic uniform and subsonic-supersonic inflows

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2024-10-011

PRE

Experimental study of combustion efficiency and outlet temperature distribution characteristics of a combined evaporative flameholder

APPLIED THERMAL ENGINEERING

IF6.9

2024-09-013

PRE

Integrating Microseismic Monitoring for Predicting Water Inrush Hazards in Coal Mines

IF3

2024-04-200

OA

Inlet Mach number ratio and static temperature ratio coupling effect on vortex structure characteristics downstream of the flameholder in subsonic-supersonic mixing flow

PHYSICS OF FLUIDS

IF4.3

2024-01-185

OA

Heat transfer characteristics of H2/air rotating detonation combustor

PHYSICS OF FLUIDS

IF4.3

2024-01-175

PRE

Combustion and emission performance of swirling-flow single trapped vortex combustor

旋流单涡燃烧室燃烧与排放性能研究

APPLIED THERMAL ENGINEERING

IF6.9

2024-01-0113

PRE

Study of the characteristics and combustion efficiency of liquid kerosene/oxygen-enriched air rotating detonation wave with different modes

IF7.5

2024-01-0111

PRE

Experimental study on the characteristics of a novel aerodynamic wake width flameholder

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2023-12-015

PRE

Wave mode analysis of a turbine guide vane-integrated rotating detonation combustor based on instantaneous frequency identification

IF9.4

2023-12-017

PRE

Inlet static pressure ratio effect on vortex structure downstream of the flameholder in subsonic-supersonic mixing flow

PHYSICS OF FLUIDS

IF4.3

2023-09-268

PRE

Ignition process of a novel swirling-flow single trapped vortex combustor with RP-3 liquid aviation fuel

IF7.5

2023-09-014

PRE

Investigations of the effect of the primary hole on ignition performance of a three-dome model combustor with RP-3 liquid aviation fuel

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2023-08-0110

PRE

Flame stability optimization of cavity primary air-jet form in an augmentor

增强器中腔主喷气形式的火焰稳定性优化

IF9.4

2022-01-0110

PRE

Spark ignition and stability limits of spray kerosene flames under subatmospheric pressure conditions (vol 114, 106734, 2021)

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-10-010

PREAI

Combustion performance in a cavity-based combustor under subatmospheric pressure

IF7.5

2021-10-0128

PREAI

Spark ignition and stability limits of spray kerosene flames under subatmospheric pressure conditions

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-07-0128

PREAI

Effect of non-uniform inlet profile on the combustion performance of an afterburner with bluff body

IF9.4

2021-02-0132

PREAI