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