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Xingliang Chen

National Key Laboratory of Solid Rocket Propulsion

H指数:6

被引数:127

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Coupling of isolator flow with heat release rate and equivalence ratio oscillations in the dual-mode scramjet

双模态 scramjet 中隔离段流与热释放速率及当量比振荡的耦合

Combustion and Flame

IF6.2

2025-10-300

PRE

Study on heat release characteristics of the dual composite flame stabilizers for the dual-mode scramjet

双模式超燃冲压发动机双复合稳焰器的放热特性研究

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2025-02-011

PRE

Experimental study on ignition and blowout characteristics of dual combined flame stabilizers in scramjet

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2023-11-019

PRE

A hybrid vapor chamber heat sink incorporating a vapor chamber and liquid cooling channel with outstanding thermal performance and hydraulic characteristics

一种混合蒸汽室散热器，结合蒸汽室和液体冷却通道，具有出色的热性能和液压特性

ENERGY CONVERSION AND MANAGEMENT

IF10.9

2021-09-0123

PRE

Modeling and experimental analysis of U-shaped segmented unidirectional heat pipe array cogeneration unit

CASE STUDIES IN THERMAL ENGINEERING

IF6.4

2021-08-016

OAAI

Modeling and experimental analysis of an internally-cooled vapor chamber

ENERGY CONVERSION AND MANAGEMENT

IF10.9

2021-05-0118

PREAI

Experimental investigation of the heat transfer performance of a novel double independent chambers casing heat pipe applied for heat dissipation at low temperatures

APPLIED THERMAL ENGINEERING

IF6.9

2021-04-017

PREAI