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arXiv · 2503.24052

Accelerated Airfoil Design Using Neural Network Approaches

Anantram Patel·Nikhil Mogre·Mandar Mane·Jayavardhan Reddy Enumula·Vijay Kumar Sutrakar
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Abstract

In this paper, prediction of airfoil shape from targeted pressure distribution (suction and pressure sides) and vice versa is demonstrated using both Convolutional Neural Networks (CNNs) and Deep Neural Networks (DNNs) techniques. The dataset is generated for 1600 airfoil shapes, with simulations carried out at Reynolds numbers (Re) ranging from 10,000 and 90,00,000 and angles of attack (AoA) ranging from 0 to 15 degrees, ensuring the dataset captured diverse aerodynamic conditions. Five different CNN and DNN models are developed depending on the input/output parameters. Results demonstrate that the refined models exhibit improved efficiency, with the DNN model achieving a multi-fold reduction in training time compared to the CNN model for complex datasets consisting of varying airfoil, Re, and AoA. The predicted airfoil shapes/pressure distribution closely match the targeted values, validating the effectiveness of deep learning frameworks. However, the performance of CNN models is found to be better compared to DNN models. Lastly, a flying wing aircraft model of wingspan >10 m is considered for the prediction of pressure distribution along the chordwise. The proposed CNN and DNN models show promising results. This research underscores the potential of deep learning models accelerating aerodynamic optimization and advancing the design of high-performance airfoils.

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Anantram Patel, Nikhil Mogre, Mandar Mane, Jayavardhan Reddy Enumula, Vijay Kumar Sutrakar. 2025-03-31. Accelerated Airfoil Design Using Neural Network Approaches. https://arxiv.org/abs/2503.24052

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