Dynamic Multimode Response of Composite Plates to Sonic Boom and Blast Loadings
Journal of Aircraft, Vol. 45, No. 2, Mart 2008, s. 498-507, ISSN: 0021-8669
DOĞAN VEDAT ZİYA
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Vibration of anti symmetric angle ply composite plates under random excitation
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 5, Eylül 2007, s. 475-484, ISSN: 0002-2667
DOĞAN VEDAT ZİYA
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Vibrational genetic algorithm as a new concept in airfoil design
Aircraft Engineering and Aerospace Technology, Vol. 74, No. 3, Haziran 2002, s. 228-236, ISSN: 0002-2667
HACIOĞLU ABDURRAHMAN,OZKOL İBRAHİM
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Bending of Composite Cylindrical Shells with Circular Cutouts: Buckling and Failure Analysis
JOURNAL OF AIRCRAFT, Vol. 56, No. 4, Temmuz 2019, s. 1551-1564, ISSN: 0021-8669
ÇELEBİ MANSUR,GÜRDAL ZAFER,BLOM-SCHİEBER AGNES,WANTHAL STEVEN,RASSAİAN MOSTAFA,TATTİNG BRİAN,TÜRKMEN HALİT SÜLEYMAN
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Optimization of the PD coefficient in a flight simulator control via genetic algorithms
Aircraft Engineering and Aerospace Technology, Vol. 74, No. 2, Nisan 2002, s. 147-153, ISSN: 0002-2667
YURT SAİT,OZKOL İBRAHİM,KAYA METİN ORHAN,HACIZADE CENGİZ
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The stability dependence on the different pressure gradients in a channel flow
Aircraft Engineering and Aerospace Technology, Vol. 75, No. 5, Ekim 2003, s. 485-490, ISSN: 0002-2667
SÖYLEMEZ HARUN TAYFUN,OZKOL İBRAHİM
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UAV-based evaluation of morphological changes induced by extreme rainfall events in meandering rivers
PLOS ONE, Vol. 15, No. 11, Ocak 2020, ISSN: 1932-6203
AKAY SEMİH SAMİ,ÖZCAN ORKAN,BALIK ŞANLI FUSUN,GÖRÜM TOLGA,ŞEN ÖMER LÜTFİ,BAYRAM BÜLENT
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Thermal Stress Concentration in Plates from Different Materials
Journal of Aircraft, Vol. 49, No. 3, Mayıs 2012, s. 941-946, ISSN: 0021-8669
ABDULALİYEV Z, BAKİOGLU M, ATAOGLU S, KURTKAYA Z, GULLUOGLU AN
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Formal intent based Flight Management System design for unmanned aerial vehicles
2014 International Conference on Unmanned Aircraft Systems (ICUAS), Orlando, FL/AMERİKA BİRLEŞİK DEVLETLERİ, 27 Mayıs 2014
TARHAN FARABİ AHMED,KOYUNCU EMRE,HASANZADE MEHMET,ÖZDEMİR UĞUR,İNALHAN GÖKHAN
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Estimated Time of Arrival Sensitivity to Aircraft Intent Uncertainty
5th IFAC Symposium on Control in Transportation Systems CTS 2018, Genoa/İTALYA, Vol. 51, No. 9, 6 Haziran 2018, s. 162-167
CASADO ENRİQUE, CİVİTA MARCO LA, UZUN MEVLÜT, KOYUNCU EMRE, İNALHAN GÖKHAN
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Boundary Moment Control of Free Vibration of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
8th Ankara International Aerospace Conference, ANKARA/TÜRKİYE, 10 Eylül 2015
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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Active Vibration Control of Aircraft Wings Modeled as Thin-Walled Composite Beams Using Piezoelectric Actuation
ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers Digital Collection, MONTREAL/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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Inner outer matching solution of Blasius equation by DTM
Aircraft Engineering and Aerospace Technology, Vol. 77, No. 4, Ağustos 2005, s. 298-301, ISSN: 0002-2667
ARIKOĞLU AYTAÇ,OZKOL İBRAHİM
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Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, California, USA/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN,EKEN SEHER,KAYA METİN ORHAN
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Boundary Moment Control of Free Vıbratıon of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
8th Ankara International Aerospace Conference, ankara/TÜRKİYE, 10 Eylül 2015
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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AEROELASTIC RESPONSE OF AN AIRCRAFT WING MODELED AS A THIN-WALLED COMPOSITE BEAM
ASME-IMECE2013, International Mechanical Engineering Congress & Exposition, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 14 Kasım 2013
EKEN SEHER, KAYA METİN ORHAN
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Applications of Metal Additive Manufacturing in Aircraft Components
1st International Conference on Smart Innovation in Science and Engineering, Salalah/UMMAN, 7 Nisan 2021, s. 30-31
YILDIZ RAŞİD AHMED
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Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections
Thin-Walled Structures, Vol. 139, Haziran 2019, s. 362-371, ISSN: 0263-8231
EKEN SEHER
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Exergetic Sustainability Indicators as a Tool in Commercial Aircraft A Case Study for a Turbofan Engine
International Journal of Green Energy, Vol. 12, No. 1, Eylül 2015, s. 28-40, ISSN: 1543-5075
AYDIN HAKAN,TURAN ÖNDER,KARAKOÇ TAHİR HİKMET,MİDİLLİ ADNAN
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Approximate Analytical Solutions Of Nonlinear Flutter Of Aircraft Wings
IFASD 2011, 15th International Forum on Aeroelasticity and Structural Dynamics, Paris/FRANSA, 26 Haziran 2011
EKEN SEHER, KERKİ TİLBE, KAYA METİN ORHAN
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