Melin Şahin

E-mail

msahin@metu.edu.tr

Department

Department of Aerospace Engineering

ORCID

0000-0001-9836-6358

Scopus Author ID

7101877767

Web of Science Researcher ID

U-5982-2018

High Aspect Ratio Composite Wings: Geometrically Nonlinear Aeroelasticity, Multi-Disciplinary Design Optimization, Manufacturing, and Experimental Testing Farsadi, Touraj; Ahmadi, Majid; Şahin, Melin; Haddad Khodaparast, Hamed; Kayran, Altan; Friswell, Michael I. (2024-03-01) In the field of aerospace engineering, the design and manufacturing of high aspect ratio composite wings has become a focal point of innovation and efficiency. These long, slender wings, constructed with advanced materials...
Boşta Hareket Davranışı İçeren Kontrol Yüzeylerine Sahip Bir Uçağın Doğrusal Olmayan Aeroservoelastik Modellenmesi ve Analizi Yurtsever, Utku; Kayran, Altan; Şahin, Melin (2022-09-18)
BİR ESNEK SAVAŞ UÇAĞI KANAT YÜKLERİNİN VEKİL MODELLER KULLANILARAK BELİRLENMESİ Zafer, Özgür; Şahin, Melin (2022-09-16)
BASINÇ TAHRİKİ İLE ŞEKİL DEĞİŞTİREN HÜCRE YAPISI TASARIMI VE ANALİZİ Köksal, Buğra; Şahin, Melin (2022-09-16)
KUVARS SARKAÇLI İVMEÖLÇER VE OKUMA DEVRESİ SİSTEM DİNAMİĞİNİN KARAKTERİZASYONU Özmen, Hasan Baran; Şahin, Melin; Özgen, Gökhan Osman (2022-09-15)
KOMPOZİT YAPILARDA BİRBİRİNE BAĞLI GLOBAL-LOKAL SONLU ELEMANLAR YÖNTEMİ İLE KATMANLAR ARASI İLERLEMELİ HASAR MODELLEMESİ Değerliyurt, Boray; Şahin, Melin (2022-09-15)
KATLANABİLİR FÜZE KANADININ DİRENGENLİK KISTASINA GÖRE YAPISAL ENİYİLEMESİ Ürün, Ata; Şahin, Melin; Gürses, Ercan (2022-09-14)
TOPOLOJİ OPTİMİZASYONU VE EKLEMELİ İMALAT İLE HAFİFLETİLEN BİR İNSANSIZ HAVA ARACI PİLON BAĞLANTI PARÇASININ KALİFİKASYONU Yılmaz, Fatih; Gürses, Ercan; Şahin, Melin (2022-09-13)
Weight reduction of an unmanned aerial vehicle pylon fitting by topology optimization and additive manufacturing with electron beam melting Yilmaz, Fatih; Şahin, Melin; Gürses, Ercan (2021-12-01) The operating altitudeof unmanned aerial vehiclescan be affected by many parameters. Lightening the structural parts to achieve targetaltitudeis one of the design efforts. Weight reductioncan beachiev...
Vibration control of a smart piezo beam via gain scheduling H-infinity controller based on LPV model TURAN, ABDULLAH; Şahin, Melin; ONAT, CEM (2021-01-01) In this study, a gain scheduling H-infinity controller based on Linear Parameter Varying (LPV) model was designed and applied to suppress the first out of plane bending vibration of a variable parameter smart beam equipped...

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