Evaluation of critical parameters in the design of a trainer aircraft landing gear
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
ÇETİNKAYA BURHAN,OZKOL İBRAHİM
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Error analysis and motion determination of a flight simulator
Aircraft Engineering and Aerospace Technology, Vol. 76, No. 2, Nisan 2004, s. 185-192, ISSN: 0002-2667
YURT SAİT,OZKOL İBRAHİM,HACIZADE CENGİZ
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Transonic airfoil design and optimisation by using vibrational genetic algorithm
Aircraft Engineering and Aerospace Technology, Vol. 75, No. 4, Ağustos 2003, s. 350-357, ISSN: 0002-2667
HACİOGLU ABDURRAHMAN,OZKOL İBRAHİM
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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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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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Aircraft icing detection, identification and reconfigurable control based on Kalman filtering and neural networks
AIAA Atmospheric Flight Mechanics Conference and Exhibit, 6220, 15 Ağustos 2005
AYKAN RAHMİ,HACIZADE CENGİZ,ÇALIŞKAN FİKRET
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Simulation-based dynamic model and speed controller design of a small-scale turbojet engine
Aircraft Engineering and Aerospace Technology, Vol. 90, No. 2, Mart 2018, s. 351-358, ISSN: 1748-8842
YAZAR IŞIL,KIYAK EMRE,ÇALIŞKAN FİKRET,KARAKOÇ TAHİR HİKMET
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Application of Weibull Distribution Method for Aircraft Component Life Estimation in Civil Aviation Sector
Journal of Traffic and Logistic Engineering, Temmuz 2017
FİDANOĞLU MELİH,GUNGOR UFUK,OZKOL İBRAHİM,KÖMÜRGÖZ KIRIŞ GÜVEN
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Comparison of modified Karnik-Mendel algorithm-based interval type-2 ANFIS and type-1 ANFIS
Aircraft Engineering and Aerospace Technology, Vol. 93, Ocak 2021, ISSN: 1748-8842
OZKOL İBRAHİM, ÖZTÜRK MUHAMMET
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Using the dynamic mesh method for genetically obtained wing structures
Aircraft Engineering and Aerospace Technology, Vol. 76, No. 3, Haziran 2004, s. 314-319, ISSN: 0002-2667
VATANDAŞ OSMAN ERGÜVEN,OZKOL İBRAHİM,KAYA METİN ORHAN
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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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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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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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Vibration response analysis of an aircraft structure in terms of crashworthiness by using differential transformation method
Gazi University Journal of Science, Vol. 37, Aralık 2024, ISSN: 2147-1762
SOYSAL AYSUN,ÖZKOL İBRAHİM,UZAL EROL
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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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Free vibration analysis of a rotating double tapered beam with flexible root via differential quadrature method
Aircraft Engineering and Aerospace Technology, Vol. 93, Ocak 2021, ISSN: 1748-8842
OZKOL İBRAHİM, YAVUZ MUSTAFA TOLGA
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A Novel Approach for Internet of Things Based Intelligent Weather Data Acquisition in Aircraft
Fifth International Symposium on Engineering, Artificial Intelligence and Applications (ISEAIA 2017), 1 Kasım 2017
SIRT DOĞU,SIRT MERVE,DAĞLARLI EVREN,ARIBAŞ ERKE
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Design of a Low-Cost Aircraft Structural Material Based on Epoxy: Recycled Rubber Composites Modified with Multifunctional Nano Particles
Annual Conference of the Society for Experimental Mechanics 2019, RENO/AMERİKA BİRLEŞİK DEVLETLERİ, 3 Haziran 2019, s. 73, ISSN: 21915652 21915644
İREZ ALAEDDİN BURAK,BAYRAKTAR EMİN
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Devulcanized rubber based composite design reinforced with nano silica, graphene nano platelets (GnPs) and epoxy for “aircraft wing spar” to withstand bending moment
Annual Conference Society for Experimental Mechanics 2018, 4 Haziran 2018, s. 9, ISSN: 21915652 21915644
İREZ ALAEDDİN BURAK,BAYRAKTAR EMİN,MİSKİOGLU İBRAHİM
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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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