Model based collaborative design & optimization of blended wing body aircraft configuration: AGILE EU project

Novel configuration design choices may help achieve revolutionary goals for reducing fuel burn, emission and noise, set by Flightpath 2050. One such advance configuration is a blended wing body. Due to multi-diciplinary nature of the configuration, several partners with disciplinary expertise collaborate in a Model driven ‘AGILE MDAO framework’ to design and evaluate the novel configuration. The objective of this research are : - To create and test a model based collaborative framework using AGILE Paradigm for novel configuration design & optimization, involving large multinational team. Reduce setup time for complex MDO problem. - Through Multi fidelity design space exploration, evaluate aerodynamic performance - The BWB disciplinary analysis models such as aerodynamics, propulsion, onboard systems, S&C were integrated and intermediate results are published in this report

Обзор по задачам динамического нагружения и оптимизации многокомпонентных тел и процессов в технологических системах

В работе сделан обзор по задачам динамического контактного нагружения и оптимизации многокомпонентных конструкций и процессов в технологических системах. Изложена классификация подходов к решению задач анализа и оптимизации для тел многокомпонентной структуры. Изучено состояние области исследований, касающейся сложного контактного динамического нагружения и оптимизации конструкции подшипниковых узлов качения