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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Solid rocket motor design using a surrogate model
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 90, No. 7, Ekim 2018, s. 1104-1127, ISSN: 1748-8842
TOLA CEYHUN,NİKBAY MELİKE
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Reliability based aeroelastic optimization of a composite aircraft wing via fluid structure interaction of high fidelity solvers
IOP Conference Series: Materials Science and Engineering, Vol. 10, No. 1, Temmuz 2010, s. 12037, ISSN: 1757-899X
NİKBAY MELİKE,NECATİ FAKKUSOGLU,MUHAMMED NASİF KURU
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Optimization of Aircraft Utilization by Reducing Scheduled Maintenance Downtime
10th Annual AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, FORT WORTH/AMERİKA BİRLEŞİK DEVLETLERİ, 13 Eylül 2010
ŞENTÜRK CANER, KAVSAOĞLU MEHMET, NİKBAY MELİKE
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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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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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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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Numerical Investigations on Low-Speed Aerodynamic Characteristics of Generic Unmanned Combat Aerial Vehicle Configurations
American Institute of Aeronautics and Astronautics (AIAA) Journal of Aircraft, Vol. 60, No. 6, Kasım 2023, ISSN: 0021-8669
ALEİSA HASSAN, KONTİS KONSTANTİNOS, NİKBAY MELİKE
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Ses-Ustu Bir Ucak Modelinin Govdesi icin Sonik Patlama Op- timizasyonu (Sonic Boom Minimization of a Supersonic Aircraft Fuselage)
8. Ulusal Havacilik ve Uzay Konferansi, Ankara/TÜRKİYE, 9 Eylül 2020
YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF, 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 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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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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Multidisciplinary Code Coupling for Analysis and Optimization of Aeroelastic Systems
AIAA Journal of Aircraft, Vol. 46, No. 6, 2009, s. 1938-1944
NİKBAY MELİKE,LEVENT ONCU,AHMET AYSAN
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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 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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Integrating Analytical Aeroelastic Instability Analysis into Design Optimiza tion of Aircraft Wing Structures
TWMS Journal of Applied and Engineering Mathematics, Vol. 1, No. 2, 2011, s. 237-253
NİKBAY MELİKE,PİNAR ACAR
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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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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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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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