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Trajectory prediction for fighter aircraft ground collision avoidance based on the model predictive control technique 基于模型预测控制技术的战斗机地面防撞轨迹预测
Q3 Earth and Planetary Sciences Pub Date : 2024-05-15 DOI: 10.1007/s42401-024-00300-6
Shiyi Yuan, Qifu Li, Bei Lu, Xingjie Niu, Yishu Liu, Wei Gao
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引用次数: 0
Initial gap modeling for wing assembly analysis 机翼装配分析的初始间隙建模
Q3 Earth and Planetary Sciences Pub Date : 2024-05-15 DOI: 10.1007/s42401-024-00302-4
Nadezhda I. Zaitseva, S. Lupuleac, J. Shinder
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引用次数: 0
A survey on synthetic jets as active flow control 关于作为主动流控制的合成射流的调查
Q3 Earth and Planetary Sciences Pub Date : 2024-05-08 DOI: 10.1007/s42401-024-00301-5
D. Sai Naga Bharghava, Tamal Jana, Mrinal Kaushik

Synthetic jets (SJs) are becoming increasingly popular in aerospace engineering due to their potential applications in flow mixing enhancement, boundary layer control, and thermal load reduction. These pulsating jets involve the periodic motion of fluid in and out of a cavity through an orifice generated by a vibrating diaphragm at the cavity base. SJs are unique because they comprise working fluid and do not require an external fluid source, setting them apart from conventional flow control techniques. Although the net mass flux is zero in a complete cycle, there is a finite net momentum flux due to the imbalanced flow conditions across the orifice, and hence SJs are also known as Zero Net Mass Flux (ZNMF) jets. Numerous experimental and numerical studies have evaluated the efficacy of SJs in controlling the flow and heat transfer characteristics under various conditions, including quiescent and cross-flow situations. This review provides a comprehensive overview of the progress in synthetic jet applications in the last 40 years, specifically focusing on their potential use in flow control, heat transfer, and related applications in aerospace engineering. The strengths and limitations of SJs are discussed, and critical areas are identified for future research and development, including further optimization and refinement of these unique jets.

由于合成射流(SJ)在流动混合增强、边界层控制和减少热负荷方面的潜在应用,其在航空航天工程中越来越受欢迎。这些脉动喷流涉及流体通过空腔底部振动膜片产生的孔口进出空腔的周期性运动。SJ 的独特之处在于它由工作流体组成,不需要外部流体源,因此有别于传统的流量控制技术。虽然在一个完整的循环中,净质量通量为零,但由于孔口处的不平衡流动条件,存在有限的净动量通量,因此 SJ 也被称为零净质量通量 (ZNMF) 喷射。大量实验和数值研究评估了 SJ 在各种条件下(包括静止和交叉流情况)控制流动和传热特性的功效。本综述全面概述了合成射流在过去 40 年中的应用进展,特别侧重于其在航空航天工程中的流动控制、热传递和相关应用的潜在用途。文中讨论了 SJ 的优势和局限性,并确定了未来研发的关键领域,包括进一步优化和改进这些独特的射流。
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引用次数: 0
Deconvolution of mode composition beamforming for rotating source localization 用于旋转源定位的模式组成波束成形解卷积
Q3 Earth and Planetary Sciences Pub Date : 2024-05-06 DOI: 10.1007/s42401-024-00297-y
Ce Zhang, Wei Ma
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引用次数: 0
Computational study on effect of free-stream turbulence on bio-inspired corrugated airfoil at different sections at low Reynolds number 低雷诺数条件下自由流湍流对不同截面生物波纹翼面影响的计算研究
Q3 Earth and Planetary Sciences Pub Date : 2024-05-02 DOI: 10.1007/s42401-024-00296-z
N. S. Divyasharada, Vikas Kumar, Ganapati N. Joshi
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引用次数: 0
Quantitative analysis of hazardous areas in a micro downburst 3D wind field 微降温三维风场中危险区域的定量分析
Q3 Earth and Planetary Sciences Pub Date : 2024-04-29 DOI: 10.1007/s42401-024-00288-z
Wenrui Jin, Tao Zhang, Xiaoxiao Lv, Jiaxue Li, Wei Li, Fandong Meng

Microburst is a common low-level wind shear weather, and it seriously threatens the safety of civil aviation flights. It is characterized by suddenness, short duration, small scale and large intensity, which leads to difficulties in accurately obtaining real data, in real-time assessing the degree of harm. In this paper, based on the characteristics of microburst, according to computational fluid dynamics, taking into account the changes of temperature and pressure with height, establish a three-dimensional wind field simulation model, and verify the validity of the model by experimental data. Using the F-factor, construct the quantitative model of each position in the wind shear region, and analyze the danger degree of the micro downwash storm flow. Investigate the influence of inlet velocity, inlet height and inlet diameter on the hazard radius, and the simulation results show that the hazard radius increases logistically with the decrease of altitude, and when the inlet velocity increases by 5 m/s or the inlet height increases by 80 m, the hazard radius increases by about 10% on average. The method of this paper can provide a new way to quantitatively analyze the wind field characteristics of micro downburst storms.

微爆是一种常见的低空风切变天气,严重威胁民航飞行安全。其特点是突发性强、持续时间短、尺度小、强度大,导致难以准确获取真实数据,实时评估危害程度。本文根据微爆的特点,依据计算流体力学,考虑温度和压力随高度的变化,建立三维风场模拟模型,并通过实验数据验证模型的有效性。利用 F 因子,构建风切变区域各位置的定量模型,分析微下沉暴流的危险程度。研究入口速度、入口高度和入口直径对危险半径的影响,模拟结果表明,危险半径随高度的降低而增加,当入口速度增加 5 m/s 或入口高度增加 80 m 时,危险半径平均增加约 10%。本文的方法为定量分析微小骤降风暴的风场特征提供了一种新的途径。
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引用次数: 0
Optimal control model as an approach to the synthesis of a supersonic transport control system 优化控制模型作为合成超音速运输控制系统的一种方法
Q3 Earth and Planetary Sciences Pub Date : 2024-04-21 DOI: 10.1007/s42401-024-00291-4
Ilias Kh. Irgaleev, Aleksandr V. Efremov, Alyona Yu. Grishina, Eugene V. Efremov
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引用次数: 0
Comparative evaluation of mathematical models of polymer composite material with the implementation of a three-dimensional stress–strain state in the simulation of impact 在冲击模拟中采用三维应力-应变状态的聚合物复合材料数学模型的比较评估
Q3 Earth and Planetary Sciences Pub Date : 2024-04-20 DOI: 10.1007/s42401-024-00286-1
Aleksandr Bolshikh, K. Shelkov, Dmitry Borovkov, Nikolay Turbin
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引用次数: 0
Comparative evaluation of the efficiency of manufacturing composite caisson panels of a wing/stabilizer for a medium-haul aircraft using automated laying and autoclave-free technologies 使用自动铺设技术和无高压釜技术制造中程飞机机翼/稳定器复合沉箱板的效率比较评估
Q3 Earth and Planetary Sciences Pub Date : 2024-04-18 DOI: 10.1007/s42401-024-00294-1
Fedor Nasonov, Pavel Milovanov, Razmik Melkonyan
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引用次数: 0
Damage prediction and failure mode analysis of composite aeroengine blade impacted by the breakstone 复合材料航空发动机叶片受碎石撞击的损伤预测和失效模式分析
Q3 Earth and Planetary Sciences Pub Date : 2024-04-16 DOI: 10.1007/s42401-024-00293-2
Xiaojing Zhang, Fangrui Yu
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引用次数: 0
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Aerospace Systems
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