Component-Based Aircraft Wing Structure Reconfiguration and Analysis on the Fly
Author:
Publisher
Elsevier BV
Reference31 articles.
1. Structural optimization of composite wings in an automated multi-disciplinary environment;T Bach;14th AIAA Aviation Technology, Integration, and Operations Conference,2014
2. A component-based hybrid reduced basis/finite element method for solid mechanics with local nonlinearities;J Ballani;Computer Methods in Applied Mechanics and Engineering,2018
3. An empirical interpolation method: application to efficient reduced-basis discretization of partial differential equations;M Barrault;Comptes Rendus Mathematique,2004
4. Multidisciplinary design optimization of aircraft wing using commercial software integration;A Benaouali;Aerospace Science and Technology,2019
5. A DoEbased approach for the implementation of structural surrogate models in the early stage design of box-wing aircraft;V Cipolla;Aerospace science and technology,2021
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