Two-Way Coupled Aero-Structural Optimization of Stable Flying Wings
An aero-structural algorithm to optimize a flying wing in cruise conditions for preliminary design is developed using two-way interaction between the structure and aerodynamics. A particle swarm routine is employed to solve the multi-objective optimization, aiming to reduce the weight of the structu...
المؤلفون الرئيسيون: | , , , , , |
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التنسيق: | مقال |
اللغة: | English |
منشور في: |
MDPI AG
2023-04-01
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سلاسل: | Aerospace |
الموضوعات: | |
الوصول للمادة أونلاين: | https://www.mdpi.com/2226-4310/10/4/346 |