DESIGN OPTIMIZATION OF VARIABLE STIFFNESS COMPOSITE LAMINATES USING SURROGATE MODELS FOR MINIMUM COMPLIANCE OF CURVED WING PANELS | AVESİS

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DESIGN OPTIMIZATION OF VARIABLE STIFFNESS COMPOSITE LAMINATES USING SURROGATE MODELS FOR MINIMUM COMPLIANCE OF CURVED WING PANELS

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İNCİ H., KAYRAN A.

11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 08 September 2021, pp.1-20, (Full Text)

Publication Type: Conference Paper / Full Text
City: Ankara
Country: Turkey
Page Numbers: pp.1-20
Middle East Technical University Affiliated: Yes