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Control of Shock Oscillations with Successive Ramps in a Hypersonic Inlet–Isolator 高超声速进气道隔振器连续匝道冲击振动控制
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-11-01 DOI: 10.1061/jaeeez.aseng-4966
Nan Li, Jialin Zheng
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引用次数: 0
Time-Varying Statistics Identification of Nonstationary Random Fluctuating Pressure via Orthogonal Polynomial Representation and Karhunen–Loève Expansion 基于正交多项式表示和karhunen - lo<e:1>展开的非平稳随机波动压力时变统计识别
4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-11-01 DOI: 10.1061/jaeeez.aseng-4672
Shaoqing Wu, Yi Zheng, Yincen Geng
A novel time domain method is proposed to estimate the time-varying statistics of nonstationary random pressure load from structural strain response samples. Orthogonal polynomials and Karhunen–Loève expansion are adopted to represent the spatial distribution of the stochastic pressure load and the random structural strain data, respectively, which transform the random pressure load identification problem to a problem of estimating a few deterministic time-varying coefficients. Numerical simulation on a plate structure subjected to nonstationary random fluctuating load is conducted to validate the proposed method, and the influence of the load’s correlation length on the identification accuracy is also discussed. To show the application perspective of the proposed method, the nonstationary gust-induced random pressure load on a wing structure is reconstructed from structural strain data. Some practical aspects, such as the number of response samples, the level of noise in the strain response, the order of orthogonal polynomial used, and the regularization method used, on the performance of the load identification method are also discussed.
提出了一种从结构应变响应样本中估计非平稳随机压力载荷时变统计量的时域方法。采用正交多项式和karhunen - lo洛夫展开分别表示随机压力载荷和随机结构应变数据的空间分布,将随机压力载荷识别问题转化为几个确定性时变系数的估计问题。通过非平稳随机波动载荷作用下的平板结构的数值模拟,验证了该方法的有效性,并讨论了载荷相关长度对识别精度的影响。为了展示该方法的应用前景,利用结构应变数据重构了机翼结构上的非平稳阵风随机压力载荷。本文还讨论了响应样本的数目、应变响应中的噪声水平、所使用的正交多项式的阶数以及所使用的正则化方法等对载荷识别方法性能的影响。
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引用次数: 0
Wide-Speed Vehicle Control Considering Flight-Propulsion Coupling Constraints 考虑飞行-推进耦合约束的高速飞行器控制
4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-11-01 DOI: 10.1061/jaeeez.aseng-5066
Shuangxi Liu, Zehuai Lin, Binbin Yan, Wei Huang, Gautam Choubey
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引用次数: 0
Nonlinear Dynamic Modeling of a Quadrotor and Its Control Using Sliding Mode Controller 四旋翼飞行器的非线性动力学建模及滑模控制器控制
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-11-01 DOI: 10.1061/jaeeez.aseng-3722
Tinu Valsa Paul, George Vadakkekara Itty, Thirunavukkarasu Indiran
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引用次数: 0
Drag Mitigation of Trilobed Airship Hull through Aerodynamic Comparison with Conventional Single-Lobed Hull 三叶飞艇船体与常规单叶船体的气动比较减阻
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-11-01 DOI: 10.1061/jaeeez.aseng-4793
M. Tripathi, M. M., Pranshul Pandey, R. Pant
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引用次数: 0
A FENN-TL Approach for Reliability Analysis of a Primary Ice Detection System 一次冰探测系统可靠性分析的FENN-TL方法
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-11-01 DOI: 10.1061/jaeeez.aseng-4599
Dinghao Yu, Zhirong Han, Bin Zhang, Fuxing Wang
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引用次数: 0
Tension Control Law for Three-Dimensional Deployment of a Geostationary Space Solar Power Station 地球静止空间太阳能电站三维展开的张力控制律
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-11-01 DOI: 10.1061/jaeeez.aseng-4963
Francisco Javier Tipan Salazar, A.F. Bertachini de Almeida Prado
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引用次数: 0
Lift and Tip Vortices Generated by Tapered Backward-Swept and Forward-Swept Wings under Stationary Ground Proximity 静止近地条件下锥形后掠翼和前掠翼产生的升力和叶尖涡
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-09-01 DOI: 10.1061/jaeeez.aseng-5054
G. Lin, T. Lee
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引用次数: 0
An Enhanced Adaptive Chirp Mode Decomposition for Instantaneous Frequency Identification of Time-Varying Structures 一种增强的自适应啁啾模式分解用于时变结构的瞬时频率识别
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-09-01 DOI: 10.1061/jaeeez.aseng-4844
Xu-Qiang Shang, Tian-Li Huang, Lei Tang, W. Ren
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引用次数: 0
Aeroelastic Design-Space Exploration for Gust-Energy Harvesting 气动弹性设计——阵风能量收集的空间探索
IF 2.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Pub Date : 2023-09-01 DOI: 10.1061/jaeeez.aseng-4769
Michael Melville, G. Bramesfeld, J. Cole, S. Miller
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引用次数: 0
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Journal of Aerospace Engineering
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