陈苏杭 (Suhang Chen)

Northwest University副教授

H指数:20

被引数:1,286

个人简介

任职于南京理工大学，研究方向为含能材料燃烧性能的微纳结构精准调控，开发高催化性-高能-钝感铝热型燃烧催化剂，以及微波点火系统、微波高能点火药、微波敏化HMX等微波含能材料。教育经历：2015年9月至2021年，于南京理工大学攻读兵器科学与技术专业博士学位。

教育背景

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工作经历

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荣誉奖项

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Microwave-Activatable Heterointerfaces With B/N-Regulated Carbon Nitride Bridge for Coupling Microwave Absorption, Catalytic Decomposition, and Programmable Energy Release

微波活化异质界面与B/N调控的碳氮化物桥联耦合微波吸收、催化分解和可编程能量释放

Small

IF12.1

2026-10-010

PRE

Synthesis, crystal structures and catalytic performance of three 2,4,6-trinitroresorcinol-based metal complexes

三种2,4,6-三硝基间苯二酚基金属配合物的合成、晶体结构与催化性能

Journal of Molecular Structure

IF4.7

2026-08-210

PRE

3D structured vesicular (μAl/PTFE)/NC composites: Tailoring combustion performance through rapid phase transition fabrication

3D结构化囊泡(μAl/PTFE)/NC复合材料：通过快速相变制备调控燃烧性能

Defence Technology

IF5.9

2026-07-210

OAAI

Dielectric interface modification enables low-power microwave ignition of aluminum particles: Mechanisms and combustion performance evaluation

介电界面改性实现了铝颗粒的低功耗微波点火：机理与燃烧性能评估

Combustion and Flame

IF6.2

2025-11-300

PRE

Improving ignition and combustion of B/KClO4 by introducing polyethylene glycol as a surfactant

通过引入聚乙二醇作为表面活性剂来改善B/KClO4的点火和燃烧

Fuel

IF7.5

2025-11-130

PRE

Corrigendum to ’Precision-engineering burn rate modulation of solid propellants via multifunctional C3N4 catalytic implantation’ [Surface and Interfaces 74 (2025) 1–16/107697]

勘误表：‘通过多功能C3N4催化植入精密工程固体推进剂燃速调制’[Surface and Interfaces 74 (2025) 1–16/107697]

Surfaces and Interfaces

IF6.3

2025-10-090

PRE

MXene-modified SASN: A composite with broad-spectrum absorption and microwave response

MXene改性SASN：一种具有宽谱吸收和微波响应的复合材料

Materials Chemistry and Physics

IF4.7

2025-10-010

PRE

Predicting operative complexity in laparoscopic splenectomy: a validated preoperative scoring system

预测腹腔镜脾切除术的手术复杂度：一种经过验证的术前评分系统

SURGICAL ENDOSCOPY AND OTHER INTERVENTIONAL TECHNIQUES

IF2.7

2025-09-010

PRE

Enhanced synergistic catalytic effect of g-C3N4-based composite by constructing interface interaction with MgFe2O4 for thermal decomposition of ammonium perchlorate

通过构建与MgFe2O4的界面相互作用，增强g-C3N4基复合材料的协同催化效应，以促进高氯酸铵的热分解

CHEMICAL ENGINEERING JOURNAL

IF13.2

2025-06-010

PRE

Enhanced photocatalytic degradation of 2, 4-dinitrophenylhydrazine by CoWO4-decorated Eu-doped Bi5O7I microspheres

SEPARATION AND PURIFICATION TECHNOLOGY

IF9

2025-04-010

PRE

Combustion enhancement and agglomeration inhibition of HTPB/AP/Al propellants using Al@AP combined with a hydrazo-triazine derivative

使用Al @ AP与肼基三嗪衍生物组合的HTPB/AP/Al推进剂的燃烧增强和团聚抑制

COMBUSTION AND FLAME

IF6.2

2025-03-010

PRE

Novel FeOOH-decorated La-doped Bi4O5I2 microspheres for boosting photocatalysis-Fenton synergy degradation of emerging contaminants

SEPARATION AND PURIFICATION TECHNOLOGY

IF9

2025-02-010

PRE

Precise fabrication and superior combustion properties of n-B pomegranate microspheres based on a new dissolution-dispersion-coating method

CHEMICAL ENGINEERING JOURNAL

IF13.2

2024-12-010

PRE

3D printed hybrid rocket fuels with μAl core-shell particles coated with polyvinylidene fluoride and polydopamine: Enhanced combustion characteristics

3D打印的由聚偏二氟乙烯和聚多巴胺涂覆的μAl核壳颗粒的混合火箭燃料：增强的燃烧特性

DEFENCE TECHNOLOGY

IF5.9

2024-12-010

OAAI

Construction of nanoflowers combustion catalyst NiO@g-C3N4 for improving thermal decomposition performance of AP

CERAMICS INTERNATIONAL

IF5.6

2024-11-012

PRE

Construction of boron-based double-layer core-shell structure composites and their combustion energy release characteristics

硼基双层核壳结构复合材料的构建及其燃烧能量释放特性

FUEL

IF7.5

2024-09-013

PRE

Ignition performance and mechanism of Ti/CuFe2O4 composites with high microwave sensitivity

CERAMICS INTERNATIONAL

IF5.6

2024-09-010

PRE

Regulation of Catalysts on Tightly Packaged Solid Propellant Energetic Particles: High Combustion Performance with Low Temperature Sensitivity

LANGMUIR

IF3.9

2024-08-120

PRE

Thermal recombination strategy designed R-CN as active shell to improve catalyst activity

SURFACES AND INTERFACES

IF6.3

2024-08-011

PRE

Lowering the burning rate temperature coefficient of composite propellant by compensating its burning surface through thermal expansion and contraction in microstructure

CHEMICAL ENGINEERING JOURNAL

IF13.2

2024-08-012

PRE