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Structural Optimization of Composite Helicopter Rotor Blades
Date
2016-09-19
Author
Işık, Ayberk Alperen
Kayran, Altan
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URI
http://www.destechpub.com/product/proceedings-american-society-composites-thirty-first-technical-conference-composite-materials/?utm_source=listrak&utm_medium=email&utm_campaign=9_23_16
https://hdl.handle.net/11511/76673
Conference Name
American Society for Composites, 31st Technical Conference and ASTM Committee D30 Meeting, (19 - 22 Eylül 2016)
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Department of Aerospace Engineering, Conference / Seminar
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Structural optimization of composite helicopter rotor blades
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Structural optimization of a helicopter rotor blade with uniform aerodynamic surface and twist at the functional region is performed for weight minimization subject to various constraints relevant to helicopter rotor blades. The genetic algorithm based optimization is performed only for the functional region of the blade. Design variables are taken as the number of unidirectional S-glass layers in the spar cap, position of the spar web with respect to the leading edge, nose mass diameter and position of the...
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A. A. Işık and A. Kayran, “Structural Optimization of Composite Helicopter Rotor Blades,” presented at the American Society for Composites, 31st Technical Conference and ASTM Committee D30 Meeting, (19 - 22 Eylül 2016), Williamsburg, VA, 2016, Accessed: 00, 2021. [Online]. Available: http://www.destechpub.com/product/proceedings-american-society-composites-thirty-first-technical-conference-composite-materials/?utm_source=listrak&utm_medium=email&utm_campaign=9_23_16.