{"id":2,"date":"2020-09-28T13:44:07","date_gmt":"2020-09-28T13:44:07","guid":{"rendered":"https:\/\/compute.sabanciuniv.edu\/?page_id=2"},"modified":"2021-06-20T10:47:17","modified_gmt":"2021-06-20T10:47:17","slug":"composite-project","status":"publish","type":"page","link":"https:\/\/compute.sabanciuniv.edu\/index.php\/composite-project\/","title":{"rendered":"Design of composite panels"},"content":{"rendered":"\n<p>Due to their high stiffness-to-weight ratio, laminated composite structures are widely used in many fields of engineering such as aviation, automotive and ship industry. Most of the time, these laminated composite panels are exposed to dynamic forces that can cause resonances; thereby leading to excessive vibrations or even failures\/malfunctions. Since these structures can be tailored in the design process, achieving an optimum design in these structures will prevent any adverse effect during its operation.\u00a0<\/p>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" width=\"1024\" height=\"364\" src=\"https:\/\/compute.sabanciuniv.edu\/wp-content\/uploads\/2021\/06\/composite-details-1024x364.png\" alt=\"\" class=\"wp-image-2386\" srcset=\"https:\/\/compute.sabanciuniv.edu\/wp-content\/uploads\/2021\/06\/composite-details-1024x364.png 1024w, https:\/\/compute.sabanciuniv.edu\/wp-content\/uploads\/2021\/06\/composite-details-300x107.png 300w, https:\/\/compute.sabanciuniv.edu\/wp-content\/uploads\/2021\/06\/composite-details-768x273.png 768w, https:\/\/compute.sabanciuniv.edu\/wp-content\/uploads\/2021\/06\/composite-details-1536x546.png 1536w, https:\/\/compute.sabanciuniv.edu\/wp-content\/uploads\/2021\/06\/composite-details.png 1648w\" sizes=\"(max-width: 1024px) 100vw, 1024px\" \/><\/figure>\n\n\n\n<p>Until recently, constant stiffness laminated composites were mostly used in these structures, where each layer of the composite structure (each laminate) was produced using a certain fiber angle. The desired design strength and dynamic properties of these flat fibers in each layer can be optimized to increase the required performance of the part. With the recent technological advancements in manufacturing of composite materials, laminates with variable stiffness properties can be produced using curvilinear fibers within each layer. Since these laminates provide better load distribution within the structure, they can perform better both statically and dynamically compared to constant stiffness composite structures.<\/p>\n\n\n\n<blockquote class=\"wp-block-quote\"><p>Laminasyon\/Katman parametre interpolasyon y\u00f6ntemine dayal\u0131 spektral modelleme yakla\u015f\u0131m\u0131 kullan\u0131larak \u00fcretilebilir, de\u011fi\u015fken sertlikte kompozit plakalar\u0131n tasar\u0131m\u0131n\u0131n \u00e7ok ama\u00e7l\u0131 eniyilenmesi, T\u00dcB\u0130TAK 1001, 120M598, 2021-2024, PI: Bekir Bediz, Researcher: Ipek Basdogan, Advisor: Gokhan Serhat.<\/p><\/blockquote>\n\n\n\n<blockquote class=\"wp-block-quote\"><p>Kompozit yap\u0131lar\u0131n \u00fc\u00e7 boyutlu gerilme, burkulma ve dinamik davran\u0131\u015f\u0131n\u0131n y\u00fcksek do\u011fruluklu ve hesaplamal\u0131\u2002olarak verimli tahmini i\u00e7in yeni bir spektral modelleme yakla\u015f\u0131m\u0131n\u0131n geli\u015ftirilmesi ve kompozit yap\u0131 tasar\u0131m\u0131\u2002eniyilemesi, T\u00dcB\u0130TAK 3501, 118M300, 2018-2021, PI: Bekir Bediz, Researcher: Kamer Kaya, Advisor: Melih Papila.<\/p><p><\/p><\/blockquote>\n","protected":false},"excerpt":{"rendered":"<p>Due to their high stiffness-to-weight ratio, laminated composite structures are widely used in many fields of engineering such as aviation, automotive and ship industry. Most of the time, these laminated composite panels are exposed to dynamic forces that can cause resonances; thereby leading to excessive vibrations or even failures\/malfunctions. Since these structures can be tailored [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":[],"_links":{"self":[{"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/pages\/2"}],"collection":[{"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/comments?post=2"}],"version-history":[{"count":2,"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/pages\/2\/revisions"}],"predecessor-version":[{"id":2387,"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/pages\/2\/revisions\/2387"}],"wp:attachment":[{"href":"https:\/\/compute.sabanciuniv.edu\/index.php\/wp-json\/wp\/v2\/media?parent=2"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}