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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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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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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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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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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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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Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle
American Institute of Aeronautics and Astronautics (AIAA) Journal of Aircraft, Vol. 60, No. 6, Kasım 2023, ISSN: 0021-8669
ALEİSA HASSAN, KONTİS KONSTANTİNOS, PİRLEPELİ BERKAY, NİKBAY MELİKE
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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 and Multi-Disciplinary Design Optimization of A Low-Boom Supersonic Transport Aircraft
2023 AIAA Scitech Forum, National Harbor, Maryland/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Ocak 2023
NİKBAY MELİKE, KILIÇ DİLAN, ÇAKMAK ENES, TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF
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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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Development of A Sonic Boom Propagation Code For Low-Boom Supersonic Aircraft Design and Optimization
AIAA SCITECH 2023 Forum, National Harbor, Maryland/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Ocak 2023
DEMİROGLU YUSUF, NİKBAY MELİKE
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Active vibration control of a laminated composite plate subjected to blast load
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 4, Ocak 2009, s. 308-315, ISSN: 0002-2667
UYANIK HAYDAR,MECİTOĞLU ZAHİT
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Multifidelity Sonic Boom Minimization of A Supersonic Aircraft by Parametric Wing Shape Design
AIAA Scitech Forum, Tennessee (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 11 Ocak 2021
YUSUF DEMİROĞLU, YILDIZ ŞIHMEHMET, NİKBAY MELİKE
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Implementation of Propulsion System Integration Losses to a Supersonic Military Aircraft Conceptual Design
AIAA Propulsion and Energy 2021 Forum, Virtual/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ağustos 2021
KARASELVİ EMRE, NİKBAY MELİKE
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Reliability Based Design Optimisation of an Aircraft Wing Structure with High Fidelity Modelling
International Journal of Design Engineering, Vol. 3, No. 3, 2011, s. 247-259
NİKBAY MELİKE,MUHAMMET NASİF KURU,SEMRA BAYAT,NECATİ FAKKUSOGLU
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Reliability Based Aeroelastic Optimization of a Com posite Aircraft Wing via Fluid Structure Interaction of High Fidelity Solvers
Materials Science and Engineering, Vol. 10, No. 1, 2010, s. 1-10
NİKBAY MELİKE,NECATİ FAKKUSOGLU,MUHAMMET NASİF KURU
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Reliability Based Multidisciplinary Optimization of Aeroelastic Systemswith Structural and Aerodynamic Uncertainties
AIAA Journal of Aircraft, Vol. 50, No. 3, 2013, s. 798-715, ISSN: 0021-8669
NİKBAY MELİKE,MUHAMMET NASİF KURU
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Multi-objective and Gradient Based Structural Design Optimization of an Aircraft Wing
ASMDO Second International Conference on Multidisciplinary Design Optimization and Applications, 2 Eylül 2008
NİKBAY MELİKE,YANANGONUL ARDA,ONCU LEVENT,KOCAS MURAT
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A Turbulence Based Sensitivity Study on Drag Prediction of the NASA Common Research Model Aircraft
Eccomas Thematic Conference - Computational Methods in Multi-Scale, Multi-Uncertainty and Multi-Physics Problems, Porto/PORTEKİZ, 15 Temmuz 2019
OZTURK SULE,PİRLEPELİ BERKAY,YİLMAZTURK MEHMET,NİKBAY MELİKE
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Sonic boom mitigation via shape optimization using an adjoint method and application to a supersonic fighter aircraft
European Journal of Computational Mechanics, Vol. 17, No. 1, Ocak 2008, s. 217-243, ISSN: 1779-7179
MAUTE KURT, FARHAT CHARBEL, ARGROW BRİAN, NİKBAY MELİKE
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