@inproceedings{Vemuri000,
    type = {inproceedings},
    key = {Vemuri000},
    title = {Physics Informed Neural Networks for Aeroacoustic Source Estimation},
    author = {Sai Karthikeya Vemuri and Joachim Denzler},
    year = {2023},
    booktitle = {IACM Mechanistic Machine Learning and Digital Engineering for Computational Science Engineering and Technology},
    abstract = {Computational Aeroacoustics (CAA) is a critical domain within computational fluid dynamics (CFD) that focuses on understanding and predicting sound generation in aerodynamic systems. Accurate estimation of Lighthill sources, which play a pivotal role in deciphering acoustic phenomena, remains a challenging task, especially when confronted with noisy and missing flow data. This study explores the potential of Physics Informed Neural Networks (PINNs) to address these challenges and capture the complex flow dynamics inherent in CAA. The integration of PINNs in CFD has gained significant attention in recent years. PINNs blend deep learning techniques with fundamental physical principles, enabling accurate predictions and enhanced modeling capabilities. Their versatility has been demonstrated across various CFD applications, ranging from turbulence modeling to flow control optimization and mesh generation. However, their potential in the field of CAA, specifically in estimating Lighthill sources from flow data, remains largely unexplored. To investigate the effectiveness of PINNs in the context of CAA, we conduct a series of experiments using high-fidelity flow data obtained from common flow configurations, such as flow around a cylinder. Leveraging this data, we create three distinct datasets that represent different data imperfections. The first dataset involves the deliberate removal of certain data points, the second dataset incorporates the addition of random noise, and the third dataset combines both missing data and noise. By incorporating the governing Navier-Stokes equations, we train the PINNs using these three datasets. The PINNs, with their inherent capability to capture complex flow patterns, are employed to estimate the aeroacoustic source map. The predicted map obtained from the PINNs is then rigorously compared to the ground truth source map derived from the high-fidelity data. Through these experiments, we demonstrate the remarkable ability of PINNs to effectively estimate the aeroacoustic source map in the presence of noisy and missing data. This validation establishes the potential of PINNs as a powerful tool for aeroacoustic analysis and source characterization. The successful application of PINNs in this study opens up new ways for further advancements in aeroacoustics. By leveraging PINNs we can enhance noise reduction techniques, optimize design processes, and improve the overall efficiency of aerodynamic systems. In conclusion, this research showcases the potential of Physics Informed Neural Networks for accurate aeroacoustic source estimation in scenarios where data quality is compromised. These findings contribute to the growing body of knowledge in aeroacoustics and offer a pathway toward more robust and efficient analysis techniques in the field.},
    doi = {10.26226/m.64c26777632e9539aa87d58e},
    url = {https://www.utep.edu/engineering/mmlde/},
    groups = {deeplearning,pinns},
    pages = {},
}