JOURNAL OF AIRCRAFT
ISSN:0021-8669

JOURNAL OF AIRCRAFT

J AIRCRAFT
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:一般,3-6周
新锐分区:工程技术3区
年发文量:111
影响因子:2.1
JCR分区:Q2

基本信息

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。
0021-8669SCIE/Scopus收录
2.1
2
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3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
17/55
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
14/55
84
111
-容易一般,3-6周-工程技术-工程:宇航
9.5%
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
100.00%0.25%2.94%
CiteScore:5.00
SJR:0.730
SNIP:1.300
学科类别分区排名百分位
大类:Engineering
小类:Aerospace Engineering
Q1
39 / 157

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

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