AERONAUTICAL JOURNAL

AERONAUTICAL JOURNAL

AERONAUT J
影响因子:1.6
是否综述期刊:
是否预警:不在预警名单内
是否OA:
出版国家/地区:ENGLAND
出版社:Cambridge University Press
发刊时间:0
发刊频率:Monthly
收录数据库:SCIE/Scopus收录
ISSN:0001-9240

期刊介绍

The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.
《航空杂志》收录了有关飞机和航天器的研究、设计和开发、建造和操作等各个方面的原创论文。因此,征集关于飞机和航天器的研究、设计和开发、建造和操作的所有方面的论文。论文也欢迎审查,全面,最近的研究发展的结果,在任何上述主题。
年发文量 130
国人发稿量 42.98
国人发文占比 0.33%
自引率 -
平均录取率0
平均审稿周期 较慢,6-12周
版面费 US$2627
偏重研究方向 工程技术-工程:宇航
期刊官网 http://www.aerosociety.com/News/Publications/Aero-Journal
投稿链接 https://www.editorialmanager.com/AEROJ

期刊高被引文献

Coupled aeropropulsive design optimisation of a boundary-layer ingestion propulsor
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.120
Off-design performance analysis of hybridized aircraft gas turbine
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.75
Gust loads on aircraft
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.48
Impact of optimised trajectories on air traffic flow management
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.155
Design of scaled model for dynamic characteristics of stiffened cylindrical shells based on equivalent similar method
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.154
An airframe/inlet integrated full-waverider vehicle design using as upgraded aerodynamic method
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.49
Characterisation of the eddy dissipation model for the analysis of hydrogen-fuelled scramjets
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.169
The effect of alternative fuels on gaseous and particulate matter (PM) emission performance in an auxiliary power unit (APU)
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.16
Enhancement of disturbance wave amplification due to the intrinsic three-dimensionalisation of laminar separation bubbles
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.115
Impact of spanwise non-uniform discrete gusts on civil aircraft loads
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.148
On-ground lateral direction control for an unswept flying-wing UAV
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.167
Numerical study of the rotational direction effect on aerodynamic loading characteristics of shipborne helicopter rotor
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.20
Reliable flight control system architecture for agile airborne platforms: an asymmetric multiprocessing approach
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.30
A holistic engineering approach to aeronautical product development
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.51
Model update and validation of a mistuned high-pressure compressor blisk
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.149
Sun-synchronous repeat ground tracks and other useful orbits for future space missions
来源期刊:Aeronautical JournalDOI:10.1017/aer.2020.21
Analysis of mistuned forced response in an axial high-pressure compressor rig with focus on Tyler–Sofrin modes
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.163
Experimental investigation of the flow structures over a 40° swept wing
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.118
Semantics-based summarisation of ATM information: Managing information overload in pilot briefings using semantic data containers
来源期刊:Aeronautical JournalDOI:10.1017/aer.2019.74
HALE wing experiments and computational models to predict nonlinear flutter and dynamic response
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.38
Sensitivity analysis of potential capacity and safety of flow corridor to self-separation parameters
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.116
A study of accidental impact scenarios for composite wing damage tolerance evaluation
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.152
Experimental determination of the aerodynamic coefficients of spinning bodies
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.15
The adverse cyclic and collective pitch effect in a rotor
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.18
A Real-time On-Chip Network Architecture for Mixed Criticality Aerospace Systems
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.80
Application of Agile Model-Based Systems Engineering in aircraft conceptual design
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.53
Experimental investigation of infrared signal characteristics in a micro-turbojet engine
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.164
A methodology for preliminary sizing of a Thermal and Energy Management System for a hypersonic vehicle
来源期刊:Aeronautical JournalDOI:10.1017/aer.2019.109
Cessna Citation X simulation turbofan modelling: identification and identified model validation using simulated flight tests
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.166
Effect of scramjet inlet vortices on fuel plume elongation and mixing rate
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.45
Wind turbine wake vortex influence on safety of small rotorcraft
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.59
Verified fuselage section water impact modelling
来源期刊:Aeronautical JournalDOI:10.1017/aer.2019.110
Numerical and experimental characterisation of an aeronautic pitot probe
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.33
Turbine thermomechanical modelling during excessive axial movement and overspeed
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.162
Low Reynolds number proprotor aerodynamic performance improvement using the continuous surface curvature design approach
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.124
A linear guide-based actuation concept for a novel morphing aileron
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.35
Performance improvement of a compound helicopter rotor head by aerodynamic design optimisation of a blade-sleeve fairing
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.172
Extensive 3D analysis for fluid–structure interaction of spanwise flexible plunging wing 3D FSI Analysis for Spanwise Flexible Plunging Wing
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.5
Longitudinal and lateral aerodynamic characterisation of reflex wing Unmanned Aerial Vehicle from flight tests using Maximum Likelihood, Least Square and Neural Gauss Newton methods
来源期刊:Aeronautical JournalDOI:10.1017/aer.2019.70
Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.71
Modeling pilot mental workload using information theory
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.13
Multi-objective optimisation of semi-closed cycle engines for high-altitude UAV propulsion
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.62
Combustion instability characteristics in a dump combustor using different hydrocarbon fuels
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.19
High-frequency transition characteristics of synthetic natural gas combustion in gas turbine
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.150
Exact strip postbuckling analysis of composite plates under compression and shear
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.27
Values that form the business: evidence from airport operations in Turkey
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.168
Optimisation and analysis of efficiency for contra-rotating propellers for high-altitude airships
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.14
A proposed solution for airborne delays: linear holding
来源期刊:Aeronautical JournalDOI:10.1017/AER.2019.78
Benefit and performance impact analysis of using hydrogen fuel cell powered e-taxi system on A320 class airliner
来源期刊:Aeronautical JournalDOI:10.1017/AER.2018.156
A new hybrid control methodology for a morphing aircraft wing-tip actuation mechanism
来源期刊:Aeronautical JournalDOI:10.1017/aer.2019.106

质量指标占比

研究类文章占比 OA被引用占比 撤稿占比 出版后修正文章占比
98.46%29.58%--

相关指数

影响因子
影响因子
年发文量
自引率
Cite Score

预警情况

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时间 预警情况
2025年03月发布的2025版不在预警名单中
2024年02月发布的2024版不在预警名单中
2023年01月发布的2023版不在预警名单中
2021年12月发布的2021版不在预警名单中
2020年12月发布的2020版不在预警名单中
*来源:中科院《 国际期刊预警名单》

JCR分区

WOS分区等级:Q2区
版本 按学科 分区
WOS期刊SCI分区
WOS期刊SCI分区
WOS期刊SCI分区是指SCI官方(Web of Science)为每个学科内的期刊按照IF数值排 序,将期刊按照四等分的方法划分的Q1-Q4等级,Q1代表质量最高,即常说的1区期刊。
(2024-2025年最新版)
ENGINEERING, AEROSPACE
Q2

中科院分区

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版本 大类学科 小类学科 Top期刊 综述期刊
2025年3月最新升级版
工程技术4区
ENGINEERING, AEROSPACE 工程:宇航
4区
2023年12月升级版
工程技术4区
ENGINEERING, AEROSPACE 工程:宇航
4区
2022年12月旧的升级版
工程技术4区
ENGINEERING, AEROSPACE 工程:宇航
4区