Aeroelastic Analysis of A Tapered Aircraft Wing
4th Ankara International Aerospace Conference, ANKARA/TÜRKİYE, 10 Eylül 2007
SEHER DURMAZ, ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
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Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: part II. Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 3, Mayıs 2007, s. 231-237, ISSN: 0002-2667
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
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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
CELİK BAYRAM, EDİS FİRAT OGUZ
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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
SENGİL NEVSAN, EDİS FİRAT OGUZ
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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, 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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The effects of the use of single task-oriented maintenance concept and more accurate letter check alternatives on the reduction of scheduled maintenance downtime of aircraft
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
SENTURK CANER,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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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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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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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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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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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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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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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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Dynamic mesh and heuristic algorithms for the design of a transonic wing
Aircraft Engineering and Aerospace Technology, Vol. 78, No. 1, Ocak 2006, s. 39-44, ISSN: 0002-2667
VATANDAŞ OSMAN ERGÜVEN,OZKOL İBRAHİM
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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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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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