Topology Optimization of Aircraft Components for Increased Sustainability
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Title
Topology Optimization of Aircraft Components for Increased Sustainability
Authors
Keywords
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Journal
AIAA JOURNAL
Volume -, Issue -, Pages 1-16
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2021-08-31
DOI
10.2514/1.j060259
References
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Related references
Note: Only part of the references are listed.- On the benefits of applying topology optimization to structural design of aircraft components
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- Fatigue behaviour of additive manufactured Ti6Al4V, with as-built surfaces, exposed to variable amplitude loading
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