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Meta Heuristics for Aircraft Arrival and Departure Scheduling on Multiple Runways
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A review of in flight detection and identification of aircraft icing and reconfigurable control
PROGRESS IN AEROSPACE SCIENCES, Vol. 60, Temmuz 2013, s. 12-34, ISSN: 0376-0421
ÇALIŞKAN FİKRET,HACIZADE CENGİZ
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How does inventory performance affect operational performance? An example from US space vehicles and aircraft parts industries
2017 8th International Conference on Recent Advances in Space Technologies (RAST), İSTANBUL/TÜRKİYE, 19 Haziran 2017, s. 291-294
HANÇERLİOĞULLARI GÜLŞAH,KÖKSALMIŞ EMRAH,ÇALIŞIR FETHİ
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Micro scale synthetic jet actuator flow simulation with characteristic based split method
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 3, Ocak 2009, s. 239-246, ISSN: 0002-2667
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Multidisciplinary Code Coupling for Analysis and Optimization of Aeroelastic Systems
AIAA Journal of Aircraft, Vol. 46, No. 6, 2009, s. 1938-1944
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Micro‐scale synthetic‐jet actuator flow simulation with characteristic‐based‐split method
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 3, Mayıs 2009, s. 239-246, ISSN: 0002-2667
ÇELİK BAYRAM,EDİS FIRAT OĞUZ
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Atomistic simulation of micro scale adiabatic piston problem
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 6, Ocak 2009, s. 499-507, ISSN: 0002-2667
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Design of MPCs for a fixed wing UAV
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ÜLKER HAKAN,BAYKARA CEMAL,ÖZSOY İSMAİL CAN
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Intercomparison and assimilation of NO2 retrievals obtained from satellite SCIAMACHY aircraft and ground observations into a regional scale air quality model CMAQ DDM for the continental U S
7th International Conference on Air Quality - Science and Application, İstanbul/TÜRKİYE, 24 Mart 2009
KAYNAK BURÇAK,HU YONGTAO,MARTİN RANDALL V,RUSSELL ARMİSTEAD G
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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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Secure Communication for MUM-T: A Blockchain and Lightweight Cryptography Framework
2024 17th International Conference on Security of Information and Networks (SIN), Sydney/AVUSTRALYA, 2 Aralık 2024, s. 1-8
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Sugeno and Mamdani based Fuzzy Inference Approaches for Aircraft Pitch Control
International Conference on Mathematics and Mathematics Education (ICMME), URFA/TÜRKİYE, 11 Mayıs 2017
ÖZTÜRK MUHAMMET,BAYEZİT İSMAİL,OKUDAN MEHMET EMİN,OZKOL İBRAHİM
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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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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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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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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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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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Aircraft Brake Induced Vibrations Investigation for Gear-Walk and Brake Chatter Phenomena
VII. International Scientific and Vocational Studies Congress – Science and Engineering, Online/TÜRKİYE, 16 Aralık 2022
ALTINBAĞ ÖNER, BALKAN DEMET
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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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