TY - GEN
T1 - Machine-learning based design of nearspherical shells under external pressure
AU - Doshi, Mitansh
AU - Ning, Xin
N1 - Funding Information:
The authors gratefully acknowledge the financial support of the Pennsylvania State University.
Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.
PY - 2021
Y1 - 2021
N2 - In this paper Extreme Gradient Boost (XGBoost) based machine learning model is designed to predict the critical buckling load of near-spherical composite shells (Icosahedron). Icosahedron is under external pressure, and the effect of changing the geometry or the composite layups on the buckling load is studied in this paper. While designing a composite structure, the engineering design space is often very large. Finding possible combinations to obtain the higher buckling load could be time consuming and computationally expensive. To overcome this problem, a data-driven machine learning model is created in this paper based on the data generated from detailed finite element analyses. Based on the geometry design parameters or material design parameters, the current model predicts the buckling load with excellent accuracy. To verify and test the model an independent test data set is created for each case and then the correlation value (R2 value) or average Root Mean Square Error (RMSE) is computed.
AB - In this paper Extreme Gradient Boost (XGBoost) based machine learning model is designed to predict the critical buckling load of near-spherical composite shells (Icosahedron). Icosahedron is under external pressure, and the effect of changing the geometry or the composite layups on the buckling load is studied in this paper. While designing a composite structure, the engineering design space is often very large. Finding possible combinations to obtain the higher buckling load could be time consuming and computationally expensive. To overcome this problem, a data-driven machine learning model is created in this paper based on the data generated from detailed finite element analyses. Based on the geometry design parameters or material design parameters, the current model predicts the buckling load with excellent accuracy. To verify and test the model an independent test data set is created for each case and then the correlation value (R2 value) or average Root Mean Square Error (RMSE) is computed.
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U2 - 10.2514/6.2021-0308
DO - 10.2514/6.2021-0308
M3 - Conference contribution
AN - SCOPUS:85100299664
SN - 9781624106095
T3 - AIAA Scitech 2021 Forum
SP - 1
EP - 12
BT - AIAA Scitech 2021 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021
Y2 - 11 January 2021 through 15 January 2021
ER -