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Precise Prediction of Aerodynamic Coefficients Using Multi-Head Attention Mechanism in Convolutional Neural Networks

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dc.contributor.author Sheikh, Khoula Ali
dc.date.accessioned 2024-09-25T07:44:25Z
dc.date.available 2024-09-25T07:44:25Z
dc.date.issued 2024
dc.identifier.other 327456
dc.identifier.uri http://10.250.8.41:8080/xmlui/handle/123456789/46875
dc.description.abstract Aerodynamic parameters such as the lift coefficient (Cl ), drag coefficient (Cd), and liftto-drag ratio (Cl/Cd) are essential for evaluating airfoil performance, enabling engineers to select suitable airfoils when designing aircraft, wind turbines, etc. Wind tunnel experiments and computational fluid dynamics (CFD) are powerful methods for obtaining these parameters. However, wind tunnel experiments demand high maintenance, while CFD continuously updates solutions until convergence, making it both expensive and timeconsuming. Machine learning algorithms train on datasets and learning patterns to make predictions, offering a faster and more cost-effective alternative. In our research, we apply a machine learning algorithm, multi-head attention, within a convolutional neural network to predict these parameters under incompressible and steady flow conditions. The model helps identify stall effects, and by incorporating multi-head attention, the model extracts only the relevant features. XFLR5 software is employed to obtain baseline values for Cl , Cd, and Cl/Cd from Computational Fluid Dynamics (CFD) simulations using 500 airfoils from the UIUC Airfoil Database, at angles of attack ranging from -5 to 20 degrees, with increments of 0.25 degrees, at a Mach number of 0.3 and a Reynolds number of 50,000. Python code is utilized to generate visual representations of the airfoil shapes. The model’s performance is assessed using Mean Squared Error (MSE), demonstrating strong results. With 95% of the data used for training, the MH-CNN achieves MSE values of 0.000283 for Cl , 0.000121 for Cd, and 0.000330 for Cl/Cd. When 70% of the data is used, the MSE slightly increases to 0.000402 for Cl , 0.000197 for Cd, and 0.000649 for Cl/Cd. This work represents a significant advancement in applying machine learning to aerodynamics, offering new possibilities for improving airfoil design and overall aerodynamic performance en_US
dc.description.sponsorship Supervisor Dr. Absaar Ul Jabbar en_US
dc.language.iso en_US en_US
dc.publisher (School of Interdisciplinary Engineering and Sciences(SINES),NUST, en_US
dc.subject Convolutional Neural Networks, Multi-Head Attention, Computational fluid dynamics, Aerodynamic coefficients en_US
dc.title Precise Prediction of Aerodynamic Coefficients Using Multi-Head Attention Mechanism in Convolutional Neural Networks en_US
dc.type Thesis en_US


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