AERONAUTICAL JOURNAL
ISSN:0001-9240

AERONAUTICAL JOURNAL

AERONAUT J
学科领域:工程技术
是否预警:不在预警名单内
是否OA:
录用周期:较慢,6-12周
新锐分区:工程技术4区
年发文量:130
影响因子:1.6
JCR分区:Q2

基本信息

《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。
0001-9240SCIE/Scopus收录
1.6
1.6
2026年3月发布
点击查看历史分区趋势    >
大类学科小类学科Top期刊综述期刊
工程技术4区
ENGINEERING, AEROSPACE 工程:宇航
3区
N/A
WOS期刊SCI分区  2024-2025最新升级版
按JIF指标学科分区收集子录JIF分区JIF排名百分位
学科:ENGINEERING, AEROSPACE
SCIE
Q2
24/55
按JCR指标学科分区收集子录JCR分区JCR排名百分位
学科:ENGINEERING, AEROSPACE
SCIE
Q2
25/55
39
130
-容易较慢,6-12周-工程技术-工程:宇航
6.2%
时间预警情况
2026年03月发布的新锐学术版不在预警名单中
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
98.46%32.39%-
CiteScore:4.00
SJR:0.445
SNIP:1.136
学科类别分区排名百分位
大类:Engineering
小类:Aerospace Engineering
Q2
54 / 157

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

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