CEAS Aeronautical Journal
ISSN:1869-5582

CEAS Aeronautical Journal

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是否预警:不在预警名单内
是否OA:
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新锐分区:-
年发文量:-
影响因子:0
JCR分区:Q0(未被收录)

基本信息

CEAS航空杂志是在CEAS的保护伞下创建的,为科学家和工程师提交的优秀科学出版物提供了一个适当的平台。德国航空航天中心(DLR)和欧洲航天局(ESA)支持该杂志。该杂志致力于发表航空科学和技术所有领域的成果和发现,以及关于飞机、旋翼机和无人驾驶航空器设计和制造新发展的报告。此外,还邀请对与航空相关的特定领域的发展状况进行深入审查,并说明可能的前进道路。该杂志发表同行评审的原创文章、(特邀)评论和简短的交流。该杂志的主要内容包括:飞行物理学和空气动力学、气动弹性和结构力学、航空声学、结构和材料、飞行力学和飞行控制、系统、飞行制导、空中交通管理、通信、导航和监视、飞机和飞机设计、旋翼机和推进系统。
1869-5582Scopus收录
0
0
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WOS期刊SCI分区  2024-2025最新升级版
暂无按学科分区信息
暂无h-index数据
-
----Engineering-Aerospace Engineering
0%
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
0.00%--
CiteScore:3.60
SJR:0.413
SNIP:1.134
学科类别分区排名百分位
大类:Engineering
小类:Aerospace Engineering
Q2
58 / 157
大类:Engineering
小类:Transportation
Q2
71 / 152

期刊高被引文献

A review of acoustic imaging methods using phased microphone arrays
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00383-4
Gust load alleviation for a long-range aircraft with and without anticipation
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00362-9
Multidisciplinary analysis of subsonic stealth unmanned combat aerial vehicles
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0325-0
Static aeroelastic stiffness optimization of a forward swept composite wing with CFD-corrected aero loads
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00397-Y
Feasibility study on fixed flight-path angle descent for wide-body passenger aircraft
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0337-9
Multiple-phase trajectory optimization for formation flight in civil aviation
来源期刊:CEAS Aeronautical JournalDOI:10.1007/978-3-319-65283-2_21
Investigations of passive wing technologies for load reduction
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00393-2
Sound proofing and thermal properties of an innovative viscoelastic treatment for the turboprop aircraft fuselage
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0326-Z
Active flow separation control at the outer wing
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00402-4
Combustion noise: modeling and prediction
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00377-2
Installation: numerical investigation
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00382-5
Weight trades in the design of a composite wing box: effect of various design choices
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0321-4
Production technologies for lightweight structures made from fibre–metal laminates in aircraft fuselages
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0330-3
Exploitation of hybrid anechoic wind tunnels for aeroacoustic and aerodynamic measurements
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00385-2
Toward noise certification during design: airframe noise simulations for full-scale, complete aircraft
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00378-1
Aircraft ground operations: steps towards automation
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00390-5
Free vibration studies on plates with central cut-out
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0339-7
Comparison of microphone array measurements in the closed test section of LSWT and ETW
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00386-1
First results of LiDAR-aided helicopter approaches during NATO DVE-mitigation trials
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0354-8
GARTEUR activities on acoustical methods and experiments for studying on acoustic scattering
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0333-0
Simulation-supported aviation cyber-security risk analysis: a case study
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0331-2
Preliminary design of advanced flight control system architectures for commercial transport aircraft
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0338-8
Linearly variable chord-extension morphing for helicopter rotor blades
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-020-00477-4
Investigation and improvement of directional stability and control of a propeller-driven STOL aircraft
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00363-8
Examples on increased-order aeroservoelastic modeling
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00361-W
Advanced low-noise aircraft configurations and their assessment: past, present, and future
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00371-8
Novel liner concepts
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00380-7
Workload reduction through steering wheel control for rotorcraft
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-00360-3
Aeroelastic behaviour of a parameterised circulation-controlled wing
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0348-6
The effects of a full-aircraft aerodynamic model on the design of a tailored composite wing
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00366-5
Experimental and analytical study of an CF-PEEK Fastener all composites single-lap shear joint under static and fatigue loading
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0334-Z
Current engine noise and reduction technology
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00381-6
Multiple-phase trajectory optimization for formation flight in civil aviation
来源期刊:CEAS Aeronautical JournalDOI:10.1007/s13272-018-0329-9
The second wind-tunnel test of DLR’s multiple swashplate system
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0323-2
New concepts for cutting, surface treatment and forming of aluminium sheets used for fibre-metal laminate manufacturing
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0324-1
Electrostatic charging of an aircraft due to airborne dust particles impacts
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-00355-0
Methods and tools for the characterisation of a generic jet fuel
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00364-7
Two-stage leak detection in vacuum bags for the production of fibre-reinforced composite components
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-00357-Y
A flight demonstration for airframe noise reduction technology
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00376-3
Validation data for aircraft noise shielding prediction
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00387-0
Limits and challenges of aircraft retrofitting for noise reduction
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00370-9
Correction to: Aircraft noise generation and assessment
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00391-4
Validation of the SmartBasing aircraft rotation and retirement strategy
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-00356-Z
Conceptual design and control of twin-propeller tail-sitter mini-UAV
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00388-Z
Assessment of two fluidic actuators for active flow control on a one-sided diffuser
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-018-0336-X
Airframe noise modeling and prediction
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00375-4
Aircraft noise immission modeling
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00374-5
Overall vehicle system noise: sonic boom
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00379-0
Aircraft noise generation and assessment: executive summary
来源期刊:CEAS Aeronautical JournalDOI:10.1007/S13272-019-00384-3
Editorial for the CEAS Aeronautical Journal special edition on Smart Fixed Wing Aircraft, WP 1.2 “Load Control”
来源期刊:CEAS Aeronautical JournalDOI:10.1007/s13272-019-00418-w

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