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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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 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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Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
Applied Mechanics and Materials, Vol. 798, Ocak 2015, s. 292-296, ISSN: 1660-9336
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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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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Active vibration control of aircraft wings modeled as thin-walled composite beams using piezoelectric actuation
ASME-IMECE-2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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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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HHO Algorithm based PID Controller Design for Aircraft Pitch Angle Control System
2nd International Congress on Human-Computer Interaction, Optimization and Robotic Applications (HORA), 26 Haziran 2020
DEMİRÖREN AYŞEN, İZCİ DAVUT, EKİNCİ SERDAR
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Aeronautical Networks for In-Flight Connectivity: A Tutorial of the State-of-the-Art and Survey of Research Challenges
IEEE ACCESS, Vol. 10, Ocak 2022, ISSN: 2169-3536
CANBERK BERK
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Aircraft Brake-Induced Vibrations Investigation for Gear-Walk and Brake Chatter Phenomena
VII. International Scientific and Vocational Studies Congress – Science and Engineering, 16 Aralık 2022
ALTINBAĞ ÖNER, BALKAN DEMET
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Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
American Institute of Aeronautics and Astronautics (AIAA) Journal of Aircraft, Vol. 60, No. 2, Mart 2023, s. 410-422, ISSN: 0021-8669
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF, NİKBAY MELİKE
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Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
MDPI Algorithms, Vol. 15, No. 7, Temmuz 2022, ISSN: 1999-4893
YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, NİKBAY MELİKE
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Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
AIAA-57th Structures, Structural Dynamics, and Materials Conference, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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COMPUTATIONAL BALLISTIC IMPACT ANALYSIS OF AIRCRAFT ARMORS
Journal of Aeronautics and Space Technologies, Vol. 10, No. 1, Ocak 2017, s. 81-95, ISSN: 2148-1059
EKEN SEHER, YAVUZ ABDULKADİR, PHOENIX STUART LEIGH
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Aeroleastic analysis of a thin-walled composite aircraft wing with an external store subjected to a follower force
ASME-IMECE2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
KAÇAR AKSONGUR ALEV, EKEN SEHER, KAYA METİN ORHAN
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F-16 JET AIRCRAFT EXPLICIT MODEL FOLLOWING BASED LONGITUDINAL CONTROLLER DESIGN AND ANGLE OF ATTACK ESTIMATION
GSRD International Conference, İstanbul/TÜRKİYE, 21 Aralık 2022
KESGİN ERTÜRK GÜLŞAH, ÜSTOĞLU İLKER
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Multi-Fidelity and Multi-Disciplinary Design Optimization of A Low-Boom Supersonic Transport Aircraft
AIAA Scitech 2023, 23 Ocak 2023
NİKBAY MELİKE, KILIÇ DİLAN, ÇAKMAK ENES, TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF
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Exergo sustainability indicators of a turboprop aircraft for the phases of a flight
Energy, Vol. 58, Eylül 2013, s. 550-560, ISSN: 03605442
AYDIN HAKAN,TURAN ÖNDER,KARAKOÇ TAHİR HİKMET,MİDİLLİ ADNAN
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