AIAA JOURNAL

AIAA JOURNAL

AIAA J
影响因子:2.8
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:0
发刊频率:Monthly
收录数据库:SCIE/Scopus收录
ISSN:0001-1452

期刊介绍

This Journal is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental results. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.
本杂志致力于通过传播揭示新的理论发展和/或实验结果的原始档案研究论文来促进航天和航空科学和技术的发展。课程内容包括航空声学、空气动力学、燃烧、推进基础、流体力学和反应流、航空航天环境的基本问题、流体动力学、激光和相关现象、等离子体、研究仪器和设备、结构力学和材料、优化、热力学和热化学。还寻求以密集的方式审查上述任何主题的最新研究发展结果的论文。
年发文量 420
国人发稿量 126.76
国人发文占比 0.3%
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 https://www.aiaa.org/JournalDetail.aspx?id=3050
投稿链接

期刊高被引文献

Enhancing Model Predictability for a Scramjet Using Probabilistic Learning on Manifolds
来源期刊:AIAA JournalDOI:10.2514/1.J057069
Enriched Piston Theory for Expedient Aeroelastic Loads Prediction in the Presence of Shock Impingements
来源期刊:AIAA JournalDOI:10.2514/1.J057595
Machine-Learning-Based Detection of Aerodynamic Disturbances Using Surface Pressure Measurements
来源期刊:AIAA JournalDOI:10.2514/1.j058486
Active Flow Control Virtual Maneuvering System Applied to Conventional Airfoil
来源期刊:AIAA JournalDOI:10.2514/1.J056258
Computation of Hypersonic Flows over Flying Configurations Using a Nonlinear Constitutive Model
来源期刊:AIAA JournalDOI:10.2514/1.J057688
Experimental study of swept impinging oblique shock boundary layer interaction
来源期刊:AIAA JournalDOI:10.2514/6.2019-0340
Bilevel Programming Weight Minimization of Composite Flying-Wing Aircraft with Curvilinear Spars and Ribs
来源期刊:AIAA JournalDOI:10.2514/1.J057892
Attenuation of Flow Separation Using Herringbone Riblets at M∞=5
来源期刊:AIAA JournalDOI:10.2514/1.J057215
Lamination Parameter Interpolation Method for Design of Manufacturable Variable-Stiffness Composite Panels
来源期刊:AIAA JournalDOI:10.2514/1.J057902
Experimental Investigations of Film Cooling in a Conical Nozzle Under Rocket-Engine-Like Flow Conditions
来源期刊:AIAA JournalDOI:10.2514/1.J057486
Exergetic Drag Characteristic Curves
来源期刊:AIAA JournalDOI:10.2514/1.J057985
Shape Optimization Using the Adjoint Lattice Boltzmann Method for Aerodynamic Applications
来源期刊:AIAA JournalDOI:10.2514/1.J057955
Effect of Forcing on a Supersonic Compression Ramp Flow
来源期刊:AIAA JournalDOI:10.2514/1.J058504
Computationally Efficient Concurrent Multiscale Framework for the Nonlinear Analysis of Composite Structures
来源期刊:AIAA JournalDOI:10.2514/1.J057880
Active Separation Control at the Pylon-Wing Junction of a Real-Scale Model
来源期刊:AIAA JournalDOI:10.2514/1.J057345
Energy-Based Drag Breakdown in Compressible Flow by Wake-Plane Integrals
来源期刊:AIAA JournalDOI:10.2514/1.J058114
Three-Component Turbulence Measurements and Analysis of a Supersonic, Axisymmetric Base Flow
来源期刊:AIAA JournalDOI:10.2514/1.J057859
Quantitative Features of Wingtip Vortex Wandering Based on the Linear Stability Analysis
来源期刊:AIAA JournalDOI:10.2514/1.J057693
Aeroelastic Stability Analysis of Tailored Pretwisted Wings
来源期刊:AIAA JournalDOI:10.2514/1.j058575
Active Polynomial Chaos Expansion for Reliability-Based Design Optimization
来源期刊:AIAA JournalDOI:10.2514/1.J058020
Computational Analysis of Interaction of a Sweeping Jet with an Attached Crossflow
来源期刊:AIAA JournalDOI:10.2514/1.J057191
Efficient Aeroelastic Solution Based on Time-Spectral Fluid–Structure Interaction Method
来源期刊:AIAA JournalDOI:10.2514/1.J057628
Frequency Control of Thin Plates with Light-Activated Shape-Memory Polymers
来源期刊:AIAA JournalDOI:10.2514/1.J058273
Topology Optimization of Solid Rocket Fuel
来源期刊:AIAA JournalDOI:10.2514/1.J057807
Shock Control of a Low-Sweep Transonic Laminar Flow Wing
来源期刊:AIAA JournalDOI:10.2514/1.J058011
Application of Resonant Femtosecond Tagging Velocimetry in the 0.3-Meter Transonic Cryogenic Tunnel
来源期刊:AIAA JournalDOI:10.2514/1.J057981
Quality-Preserving Linear Elasticity Mesh Movement Algorithm for Multi-Element Unstructured Meshes
来源期刊:AIAA JournalDOI:10.2514/1.J057463
Beam Theory for Asymptotic Analysis of Aperiodic and Inhomogeneous Structures
来源期刊:AIAA JournalDOI:10.2514/1.J057563
Iterative Component Mode Synthesis Using a Priori and a Posteriori Criteria
来源期刊:AIAA JournalDOI:10.2514/1.J057661
Mode Behavior in Supersonic Cavity Flows
来源期刊:AIAA JournalDOI:10.2514/1.J057818
Enhanced Stability of Two-Material Panels in Supersonic Flow: Optimization Strategy and Physical Explanation
来源期刊:AIAA JournalDOI:10.2514/1.j057965
Review of Laminated Composite Plate Theories, with Emphasis on Variational Asymptotic Method
来源期刊:AIAA JournalDOI:10.2514/1.J057552
Mutual Effect Between Swept-and-Leaned Vanes and Acoustic Liners on Fan Interaction-Noise Reduction
来源期刊:AIAA JournalDOI:10.2514/1.J057854
Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Large-Scale Hypersonic Facility
来源期刊:AIAA JournalDOI:10.2514/1.J057759
Estimation of Inflow Uncertainties in Laminar Hypersonic Double-Cone Experiments
来源期刊:AIAA JournalDOI:10.2514/1.J059033
Multifield Variational Sectional Analysis for Accurate Stress Computation of Multilayered Composite Beams
来源期刊:AIAA JournalDOI:10.2514/1.J057384
Local Stochastic Vortex Structure Method for Synthetic Turbulence Computation in Flight Simulators
来源期刊:AIAA JournalDOI:10.2514/1.J057329
U.S. Army Rotorcraft Research at Ames: New Frontier in Dynamics and Aeroelasticity
来源期刊:AIAA JournalDOI:10.2514/1.J057503
Acoustic Excitation as Triggering Mechanism of the “DC Shift” in Hybrid Rockets
来源期刊:AIAA JournalDOI:10.2514/1.j058139
Effect of Nonequilibrium Reacting Flow on Flutter at Hypersonic Flight Speed
来源期刊:AIAA JournalDOI:10.2514/1.J057713
Validation of the Steady-State Hover Formulation for Accurate Performance Predictions
来源期刊:AIAA JournalDOI:10.2514/1.j058408
Performance Characteristics of Airfoils with Leading-Edge Tubercles and an Internal Slot
来源期刊:AIAA JournalDOI:10.2514/1.J058145
Aerodynamic Parameter Prediction via Artificial Hair Sensors with Signal Power in Turbulent Flow
来源期刊:AIAA JournalDOI:10.2514/1.J057632
Effect of Geometric Configurations on the Starting Transients in Vacuum Ejector
来源期刊:AIAA JournalDOI:10.2514/1.J058071
Structure-Based Model of a Forced Shear Layer
来源期刊:AIAA JournalDOI:10.2514/1.J057422
Effects of Perforated Liners on Controlling Combustion Instabilities in Annular Combustors
来源期刊:AIAA JournalDOI:10.2514/1.J059099
Verification of Unstructured Grid Adaptation Components
来源期刊:AIAA JournalDOI:10.2514/1.j058783
Nonlinear Modal Interactions of Swept Composite Aircraft Wings Carrying External Stores
来源期刊:AIAA JournalDOI:10.2514/1.J057582
Onset of Transient Shock Interaction with Cavity Shear Layer
来源期刊:AIAA JournalDOI:10.2514/1.J058448
Stability Analysis of the Swirling Majdalani–Fist Mean Flowfield in Solid Rocket Motors
来源期刊:AIAA JournalDOI:10.2514/1.j058568

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%--0.23%

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

查看说明
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:Q1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
Q1

中科院分区

查看说明
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
3区
2023年12月升级版
工程技术3区
ENGINEERING, AEROSPACE 工程:宇航
3区
2022年12月旧的升级版
工程技术3区
ENGINEERING, AEROSPACE 工程:宇航
2区