Abstract
An optimization strategy is presented for large composite structure based on manufacturing constraints and genetic algorithm. First, on the basis of region division and key region defined, both angle and length design variables for each ply are introduced to make laminate thickness and stacking sequence be optimized simultaneously, also considering laminate ply continuity. Finally, a composite wing is optimized using the current methodology. The result shows that the optimization method can obtain optimum design satisfying manufacturing constraints and weight reduction for large composite structure.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: DEStech Transactions on Engineering and Technology Research
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
