TY - JOUR
T1 - APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS
AU - Dinh, Quang Nguyen
AU - Tran, The Hung
AU - Sharma, Gopal
AU - Tanimoto, Jun
N1 - Publisher Copyright:
© 2024, International Council of the Aeronautical Sciences. All rights reserved.
PY - 2024
Y1 - 2024
N2 - The utilization of longitudinal grooves has demonstrated effectiveness in reducing drag on axisymmetric boattail models. However, the intricate relationship between groove parameters and drag force defies simple physical equations, necessitating the discovery of an optimal parameter set. Conventional experimental and numerical simulation approaches prove impractical due to their resource-intensive nature. Instead, Artificial Neural Networks (ANNs) offer a promising alternative. In this study, a three-layer ANN is trained using 192 examples generated by Ansys Fluent with the Reynolds-Averaged Navier-Stokes (RANS) method and the k-ω SST model. Subsequently,48 examples are employed for network validation. Comparison between ANN-predicted values and CFDdetermined drag coefficients reveals an average difference of less than 0.76%, validating the network's reliability.The ANN successfully identifies optimal groove parameters across various boattail angles, and numericalsimulations conducted on models featuring these optimal grooves further validate the ANN's accuracy in predicting drag coefficients, with a negligible deviation of only 0.98%. Additionally, analysis of flow characteristics and aerodynamics aids in understanding factors contributing to drag reduction.
AB - The utilization of longitudinal grooves has demonstrated effectiveness in reducing drag on axisymmetric boattail models. However, the intricate relationship between groove parameters and drag force defies simple physical equations, necessitating the discovery of an optimal parameter set. Conventional experimental and numerical simulation approaches prove impractical due to their resource-intensive nature. Instead, Artificial Neural Networks (ANNs) offer a promising alternative. In this study, a three-layer ANN is trained using 192 examples generated by Ansys Fluent with the Reynolds-Averaged Navier-Stokes (RANS) method and the k-ω SST model. Subsequently,48 examples are employed for network validation. Comparison between ANN-predicted values and CFDdetermined drag coefficients reveals an average difference of less than 0.76%, validating the network's reliability.The ANN successfully identifies optimal groove parameters across various boattail angles, and numericalsimulations conducted on models featuring these optimal grooves further validate the ANN's accuracy in predicting drag coefficients, with a negligible deviation of only 0.98%. Additionally, analysis of flow characteristics and aerodynamics aids in understanding factors contributing to drag reduction.
KW - Artificial Neural Network
KW - boattail
KW - drag coefficient
KW - numerical simulation
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M3 - Conference article
AN - SCOPUS:85208812813
SN - 1025-9090
JO - ICAS Proceedings
JF - ICAS Proceedings
T2 - 34th Congress of the International Council of the Aeronautical Sciences, ICAS 2024
Y2 - 9 September 2024 through 13 September 2024
ER -