AIAA JOURNAL美国航空航天学会杂志
AIAA JOURNAL(英文缩写 AIAA J),ISSN 0001-1452,eISSN 1533-385X,中文译名:美国航空航天学会杂志 是一本学术期刊。本页汇总该期刊的最新影响因子、分区信息以及最新收录于 PubMed 的文献,帮助您快速了解期刊全貌。
指标来源：jcr_cas_ifqb
期刊介绍由 AI 生成，仅供参考。
期刊简介
AIAA Journal 是航空航天领域历史悠久的核心学术期刊，由美国航空航天学会主办，聚焦空气动力学、推进、结构力学、飞行力学与控制等基础与工程交叉研究。读者群主要为航空航天工程师、力学研究者及高校师生，强调理论深度与实验验证的结合，在飞行器设计、流体物理和结构动力学方向具有较高参考价值。
研究方向
主要方向包括空气动力学与流体力学、燃烧与推进、结构动力学与材料、气动弹性、飞行力学与控制、数值模拟与实验测试方法。论文类型以原创研究长文为主，兼有综述和简短技术评论，侧重力学机理与工程应用之间的衔接。
期刊特色
研究取向偏重理论建模、数值计算与实验验证的融合，论文通常要求清晰的物理洞察和可重复的结果。篇幅较完整，适合有扎实力学基础、从事航空航天基础问题研究的学者和工程师，也适合作为研究生深入课题的参考来源。
投稿难度
投稿难度中等偏上，对创新性和力学深度要求较高，仅凭分区难以判断录用前景。建议先明确物理问题的新意，完善验证算例与对比数据，并注意英文表达和图表规范，必要时参考近期同方向论文的写作风格。
历年影响因子趋势
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AIAA JOURNAL 最新收录文献
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Active Flow Control on Vertical Tail Models.
Active flow control (AFC) subscale experiments were conducted at the Lucas Wind Tunnel of the California Institute of Technology. Tests were performed on a generic vertical tail model at low speeds. F…
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Femtosecond laser tagging in R134a with trace quantities of air.
Femtosecond laser tagging is demonstrated for the first time in R134a (1,1,1,2-Tetrafluoroethane) gas, and in mixtures of R134a with small quantities of air. A systematic study of this tagging method …
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Volterra Kernels Assessment via Time-Delay Neural Networks for Nonlinear Unsteady Aerodynamic Loading Identification.
Reduced-order modeling using the Volterra series approach has been successfully applied in the past decades to weakly nonlinear aerodynamic and aeroelastic systems. However, aspects regarding the iden…
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Towards a priori uncertainty quantification in coarse-grained molecular dynamics: Generalized multipole potentials.
In computational materials science, coarse-graining approaches often lack a priori uncertainty quantification (UQ) tools that estimate the accuracy of a reduced-order model before it is calibrated or …
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Influence of a Backward-Facing Step on Swept-Wing Boundary-Layer Transition.
Experimental measurements were performed on a swept flat-plate model with an airfoil leading edge and imposed chordwise pressure gradient to determine the effects of a backward-facing step on transiti…
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Direct Numerical Simulation Database for Hypersonic Turbulent Boundary Layers.
In this paper, we present a direct numerical simulation database of high-speed zero-pressure-gradient turbulent boundary layers developing spatially over a flat plate with nominal freestream Mach numb…
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Blunt body paradox and improved application of transient growth framework.
The "Reshotko-Tumin transition criterion" based on optimal transient growth successfully correlates laboratory measurements of roughness induced transition over blunt body configurations. Even though …
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Azimuthal Variation of Instabilities Generated on a Flared Cone by Laser Perturbations.
To study the azimuthal development of boundary-layer instabilities, a controlled, laser-generated perturbation was created in the freestream of the Boeing/U.S. Air Force Office of Scientific Research …
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Receptivity and Forced Response to Acoustic Disturbances in High-Speed Boundary Layers.
Supersonic boundary-layer receptivity to freestream acoustic disturbances is investigated by solving the Navier-Stokes equations for Mach 3.5 flow over a 7 deg half-angle cone. The freestream disturba…
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Interaction of a Backward-Facing Step and Crossflow Instabilities in Boundary-Layer Transition.
A swept flat plate model with an imposed pressure gradient was experimentally investigated in a low-speed flow to determine the effect of a backward-facing step on transition in a stationary crossflow…