L1 Adaptive Controller Design for a Tail Fin Controlled Fixed-Wing Unmanned Aerial Vehicle
13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons, Solerno/İTALYA, 5 Eylül 2023
DEMİRLİ ALİCAN,KOÇ İLKER MURAT,KÜRKÇÜ BURAK
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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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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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Aerodynamic Design Optimization of a Non-Planar C-Wing Configuration
10th Ankara International Aerospace Conference (AIAC), 18 Eylül 2019
SUKAS HULYA,PİRLEPELİ BERKAY,RAMESH KİRAN,NİKBAY MELİKE,KONTİS KONSTANTİNOS
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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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Aeroelastic Predictions for Steady and Unsteady Flow Characteristics of HIRENASD Wing
Progress in Computational Fluid Dynamics, Geneve/İSVİÇRE, Vol. 16, No. 1, Ocak 2016, s. 26-37, ISSN: 1741-5233
NİKBAY MELİKE,PİNAR ACAR
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Flutter based aeroelastic optimization of an aircraft wing with analytical approach
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 23 Nisan 2012
NİKBAY MELİKE,ACAR PİNAR
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Conceptual Design of a Non-Constant Sweep Blended Flying Wing UCAV Configuration
2022 AIAA Aviation Forum, Chicago/AMERİKA BİRLEŞİK DEVLETLERİ, 27 Haziran 2022
ALEİSA HASSAN, KONTİS KONSTANTİNOS, NİKBAY MELİKE, PİRLEPELİ BERKAY, ÇAKMAK ENES, KARA EMRE
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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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Steady and Unsteady Aeroelastic Computations of HIRENASD Wing for Low and High Reynolds Numbers
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 8 Nisan 2013
ACAR PİNAR,NİKBAY MELİKE
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Robust Aeroelastic Design Optimization of Wing Store Configurations Based on Flutter Criteria
14th AIAA/ISSMO Multidisciplinary Analysis and Optimization (MAO) Conference, Indianapolis/AMERİKA BİRLEŞİK DEVLETLERİ, 17 Eylül 2012
NİKBAY MELİKE,PİNAR ACAR
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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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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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Multidisciplinary Uncertainty Quantification in Aeroelastic Analyses of Semi Span Supersonic Transport Wing
AIAA Aviation and Aeronautics Forum and Exposition, 22 Haziran 2015
NİKBAY MELİKE,PİNAR ACAR
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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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Conceptual layout of aeroelastic wing structures by topology optimization
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver/AMERİKA BİRLEŞİK DEVLETLERİ, 22 Nisan 2002
MAUTE KURT,NİKBAY MELİKE,FARHAT CHARBEL
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AEROELASTIC RESPONSE OF AN AIRCRAFT WING MODELED AS A THIN-WALLED COMPOSITE BEAM
ASME-IMECE2013, International Mechanical Engineering Congress & Exposition, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 14 Kasım 2013
EKEN SEHER, KAYA METİN ORHAN
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Aeroleastic analysis of a thin-walled composite aircraft wing with an external store subjected to a follower force
ASME-IMECE2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
KAÇAR AKSONGUR ALEV, EKEN SEHER, KAYA METİN ORHAN
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FLUTTER ANALYSIS OF GOLAND WING VIA FINITE ELEMENT METHOD
6. ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 14 Eylül 2011
ÖZDEMİR ÖZGE, EKEN SEHER, KAYA METİN ORHAN
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Rapid Prototyping of a Fixed-Wing VTOL UAV for Design Testing
JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, Vol. 84, Aralık 2016, s. 639-664, ISSN: 0921-0296
İNALHAN GÖKHAN, OZKOL IBRAHİM, KAYA METİN ORHAN, VURUŞKAN ASLIHAN
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