Gradient-based Optimization of Postbuckled Steered-Fiber Aircraft Shell via ESLM (by T. Ungwattanapanit et. al; Technical University Munich; Germany)

Rahul_P1
Rahul_P1
Altair Employee
edited November 2023 in Altair HyperWorks

Goal: Efficient optimization of steered-fiber Airbus Sagitta UAV shell subject to pre- & postbuckling constraints

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