JOURNAL OF AIRCRAFT

JOURNAL OF AIRCRAFT

J AIRCRAFT
影响因子:2.1
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:UNITED STATES
出版社:American Institute of Aeronautics and Astronautics Inc. (AIAA)
发刊时间:1964
发刊频率:Bimonthly
收录数据库:SCIE/Scopus收录
ISSN:0021-8669

期刊介绍

This Journal is devoted to the advancement of the applied science and technology of airborne flight through the dissemination of original archival papers describing significant advances in aircraft, the operation of aircraft, and applications of aircraft technology to other fields. The Journal publishes qualified papers on aircraft systems, air transportation, air traffic management, and multidisciplinary design optimization of aircraft, flight mechanics, flight and ground testing, applied computational fluid dynamics, flight safety, weather and noise hazards, human factors, airport design, airline operations, application of computers to aircraft including artificial intelligence/expert systems, production methods, engineering economic analyses, affordability, reliability, maintainability, and logistics support, integration of propulsion and control systems into aircraft design and operations, aircraft aerodynamics (including unsteady aerodynamics), structural design/dynamics , aeroelasticity, and aeroacoustics. It publishes papers on general aviation, military and civilian aircraft, UAV, STOL and V/STOL, subsonic, supersonic, transonic, and hypersonic aircraft. Papers are sought which comprehensively survey results of recent technical work with emphasis on aircraft technology application.
该杂志致力于通过传播描述飞机、飞机的操作和飞机技术在其他领域的应用的重大进展的原始档案文件来推进机载飞行的应用科学和技术。该杂志发表合格的论文,内容涉及飞机系统、空中运输、空中交通管理、飞机的多学科设计优化、飞行力学、飞行和地面试验、应用计算流体力学、飞行安全、天气和噪音危害、人为因素、机场设计、航空公司运营、计算机在飞机上的应用,包括人工智能/专家系统、生产方法、工程经济分析、可承受性、可靠性、可维护性和后勤保障;推进系统和控制系统与飞机设计和使用的一体化;飞机空气动力学(包括非定常空气动力学);结构设计/动力学;气动弹性和气动声学。它发表有关通用航空、军用和民用飞机、UAV、STOL和V/STOL、亚音速、超音速、跨音速和高超音速飞机的论文。本文所要找的是那些综合评述近期技术工作结果的论文,重点放在飞机技术应用上。
年发文量 111
国人发稿量 10.38
国人发文占比 0.09%
自引率 -
平均录取率0
平均审稿周期 一般,3-6周
版面费 -
偏重研究方向 工程技术-工程:宇航
期刊官网 http://arc.aiaa.org/loi/ja
投稿链接

期刊高被引文献

Impact of Morphing Trailing Edges on Mission Performance for the Common Research Model
来源期刊:Journal of AircraftDOI:10.2514/1.C034967
Minimizing Induced Drag with Lift Distribution and Wingspan
来源期刊:Journal of AircraftDOI:10.2514/1.C035027
Summary of Propagation Cases of the Second AIAA Sonic Boom Prediction Workshop
来源期刊:Journal of AircraftDOI:10.2514/1.C034805
New Robust Method to Study Flight Flutter Testing
来源期刊:Journal of AircraftDOI:10.2514/1.C034863
Distributed Pressure Sensing–Based Flight Control for Small Fixed-Wing Unmanned Aerial Systems
来源期刊:Journal of AircraftDOI:10.2514/1.C035416
Aviation Noise-Pollution Mitigation Through Redesign of Aircraft Departures
来源期刊:Journal of AircraftDOI:10.2514/1.C035001
Coupled Simulations of Atmospheric Turbulence-Modified Ship Airwakes and Helicopter Flight Dynamics
来源期刊:Journal of AircraftDOI:10.2514/1.C035158
Observability and Performance Analysis of a Model-Free Synthetic Air Data Estimator
来源期刊:Journal of AircraftDOI:10.2514/1.C035290
Method for Designing Hybrid Airfoils for Icing Wind-Tunnel Tests
来源期刊:Journal of AircraftDOI:10.2514/1.C034987
Vortex-Sheet Representation of Leading-Edge Vortex Shedding from Finite Wings
来源期刊:Journal of AircraftDOI:10.2514/1.C035124
Structurally Consistent Class/Shape Transformation Equations for Morphing Airfoils
来源期刊:Journal of AircraftDOI:10.2514/1.C035025
Numerical Investigation of the Effect of Leading-Edge Tubercles on Propeller Performance
来源期刊:Journal of AircraftDOI:10.2514/1.C034845
Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag
来源期刊:Journal of AircraftDOI:10.2514/1.C034992
Structural Optimization of Internal Structure of Aircraft Wings with Curvilinear Spars and Ribs
来源期刊:Journal of AircraftDOI:10.2514/1.C034818
Stability Analysis of Tailsitters in Vertical Takeoff and Landing Flights
来源期刊:Journal of AircraftDOI:10.2514/1.C035209
Effectiveness-Based Design of an Aircraft Considering Mission Uncertainties
来源期刊:Journal of AircraftDOI:10.2514/1.C035402
Real-Time Closed-Loop System Identification of a Quadcopter
来源期刊:Journal of AircraftDOI:10.2514/1.C034219
System noise assessment of a tube-and-wing aircraft with geared turbofan engines
来源期刊:Journal of AircraftDOI:10.2514/1.C034935
Verification and Validation of OpenFOAM for High-Lift Aircraft Flows
来源期刊:Journal of AircraftDOI:10.2514/1.C034918
Complete Online Algorithm for Air Data System Calibration
来源期刊:Journal of AircraftDOI:10.2514/1.C034964
Mission Analysis and Emissions for Conventional and Hybrid-Electric Commercial Transport Aircraft
来源期刊:Journal of AircraftDOI:10.2514/1.C035070
Passive Gust Loads Alleviation in a Truss-Braced Wing Using an Inerter-Based Device
来源期刊:Journal of AircraftDOI:10.2514/1.c035452
Wind-Tunnel Study of the Autoregressive Moving-Average Flutter Prediction Method
来源期刊:Journal of AircraftDOI:10.2514/1.C035203
Aerodynamic and Aeroacoustic Effects of Swirl Recovery Vanes Length
来源期刊:Journal of AircraftDOI:10.2514/1.c035552
Aerodynamic Sails for Passive Guidance of High-Altitude Balloons: Static-Stability and Equilibrium Performance
来源期刊:Journal of AircraftDOI:10.2514/1.C035353
Dynamic Distributed Morphing Control of an Aeroelastic Wing for a Small Drone
来源期刊:Journal of AircraftDOI:10.2514/1.c035182
Blade Passage Loads and Deformation of a Coaxial Rotor System in Hover
来源期刊:Journal of AircraftDOI:10.2514/1.c035469
Sizing High-Aspect-Ratio Wings with a Geometrically Nonlinear Beam Model
来源期刊:Journal of AircraftDOI:10.2514/1.C035296
Role of Higher-Order Terms in Local Piston Theory
来源期刊:Journal of AircraftDOI:10.2514/1.C034920
Continuation Multilevel Monte Carlo Evolutionary Algorithm for Robust Aerodynamic Shape Design
来源期刊:Journal of AircraftDOI:10.2514/1.C035054
Aerodynamic Load Control for Multi-Element Airfoils Using Surface-Normal Trailing-Edge Blowing
来源期刊:Journal of AircraftDOI:10.2514/1.C035248
Improvement of Wall-Corrections at the National Research Council’s Trisonic Wind Tunnel
来源期刊:Journal of AircraftDOI:10.2514/1.c035545
Vortex Generators for Corner Separation Caused by Shock-Wave/Boundary-Layer Interactions
来源期刊:Journal of AircraftDOI:10.2514/1.C034994
Investigation of Rotor Noise Shielding Effects by the Helicopter Fuselage in Forward Flight
来源期刊:Journal of AircraftDOI:10.2514/1.C035009
Modeling-Based Hyper-Reduction of Multidimensional Computational Fluid Dynamics Data: Application to Ship Airwake Data
来源期刊:Journal of AircraftDOI:10.2514/1.c035315
Probabilistic Multimodel Ensemble Wake-Vortex Prediction Employing Bayesian Model Averaging
来源期刊:Journal of AircraftDOI:10.2514/1.C035109
Assessment of the Wake-Vortex Proximity to Landing Aircraft Exploiting Field Measurements
来源期刊:Journal of AircraftDOI:10.2514/1.C035252
Sliding Wear and Freeplay Growth due to Control Surface Limit Cycle Oscillations
来源期刊:Journal of AircraftDOI:10.2514/1.C035438
Optimal Control Approach to Helicopter Noise Abatement Trajectories in Nonstandard Atmospheric Conditions
来源期刊:Journal of AircraftDOI:10.2514/1.C034751
Hybrid Active Vibration Control of Helicopter Fuselage Driven by Piezoelectric Stack Actuators
来源期刊:Journal of AircraftDOI:10.2514/1.C034965
Experimental Studies on a Mesoscale Cycloidal Rotor in Hover
来源期刊:Journal of AircraftDOI:10.2514/1.C034736
Using Vmcg-Limited V1, Controllability Issues on Contaminated Runways and in Crosswind
来源期刊:Journal of AircraftDOI:10.2514/1.C035222
Determination of Model Structure from Flight Test with Generalized Additive Models
来源期刊:Journal of AircraftDOI:10.2514/1.C035171
Establishing unusual-weather detection system prototype using onboard sensor information
来源期刊:Journal of AircraftDOI:10.2514/1.C034630
High-Lift Simulations of the Japan Aerospace Exploration Agency Standard Model
来源期刊:Journal of AircraftDOI:10.2514/1.C035268
Fuel and Carbon Dioxide Emission Assessment for a Curved Approach Procedure
来源期刊:Journal of AircraftDOI:10.2514/1.C035379
Symmetric Versus Asymmetric Pitching of a Cycloidal Rotor Blade at Ultra-Low Reynolds Numbers
来源期刊:Journal of AircraftDOI:10.2514/1.C034776
Monolithic Approach for Next-Generation Aircraft Design Considering Airline Operations and Economics.
来源期刊:Journal of aircraftDOI:10.2514/1.C035312
Optimal Airspeeds for Scheduled Electric Aircraft Operations
来源期刊:Journal of AircraftDOI:10.2514/1.C035051
Effects of Propulsion System Operation on Military Aircraft Survivability
来源期刊:Journal of AircraftDOI:10.2514/1.C035508

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
100.00%0.25%-2.94%

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》

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WOS分区等级:Q2区
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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。
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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3区
ENGINEERING, AEROSPACE 工程:宇航
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工程技术3区
ENGINEERING, AEROSPACE 工程:宇航
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2022年12月旧的升级版
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ENGINEERING, AEROSPACE 工程:宇航
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