重建跨音速缓冲气动噪声的混合方法:随机森林和压缩传感算法的集成

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-07-08 DOI:10.1016/j.ast.2024.109379
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引用次数: 0

摘要

用于获取空气动力噪声的实验测量和数值模拟方法面临着成本高、周期长等问题。采用单一的机器学习方法预测气动噪声也需要足够的数据量。据此,本文提出了一种集成随机森林和压缩传感(RF_CS)的混合方法,以从稀疏数据中精确重建跨音速缓冲区气动噪声。首先,利用以非线性特征提取能力强而著称的 RF 算法获取基函数。然后,根据有限的传感器数据和基函数,使用 L1 优化算法计算基系数。最后,利用基函数和基系数的线性组合来重构空气动力噪声,包括功率谱密度、声压级和流动模式。与基于适当正交分解的压缩传感法(POD_CS)相比,所提出的算法能有效地将误差降低约 2-20 倍,并将模式的绝对误差降低约 2-3 个数量级。具体来说,RF_CS 方法可确保各种流动条件下的功率谱密度重建误差均低于 3E-3,实现了从一种流动条件到整个样本空间的泛化。此外,这种方法可以利用大约 10 个传感器来重建精确的声压级和模式,误差分别在 5E-3 和 5E-5 以内。这样就可以根据单个马赫数条件在整个马赫数空间内进行概括。
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A hybrid approach for reconstruction of transonic buffet aerodynamic noise: Integrating random forest and compressive sensing algorithm

Experimental measurements and numerical simulation methods for obtaining aerodynamic noise face issues such as high costs and long periods. A single machine learning method for predicting aerodynamic noise also requires a sufficient amount of data. According to this, this paper proposes a hybrid method integrating Random Forest and Compressive Sensing (RF_CS) to accurately reconstruct transonic buffet aerodynamic noise from sparse data. First, the RF algorithm, known for its strong nonlinear feature extraction capabilities, is used to obtain the basis function. Then, the basis coefficients are calculated using the L1 optimization algorithm based on limited sensor data and basis functions. Finally, a linear combination of basis functions and basis coefficients is used to reconstruct aerodynamic noise, including power spectral density, sound pressure level, and flow modes. Compared to the Compressive Sensing based on Proper Orthogonal Decomposition (POD_CS), the proposed algorithm can effectively reduce error by approximately 2–20 times and decrease the absolute error of modes by about 2–3 orders of magnitude. Specifically, the RF_CS method ensures that the reconstruction errors for power spectral density across various flow conditions are all below 3E-3, achieving generalization from one flow condition to the entire sample space. Additionally, this approach can utilize approximately 10 sensors to reconstruct accurate sound pressure level and modes, with errors within 5E-3 and 5E-5, respectively. This allows for generalization across the entire Mach number space based on a single Mach number condition.

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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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