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MULTIFIDELITY AND MULTIOBJECTIVE SURROGATE BASED DESIGN OPTIMIZATION OF UCAV WITH NON PLANAR WING CONFIGURATION
Bilişim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
BERKAY PİRLEPELİ
Melike Nikbay Tez Yüksek Lisans Devam Ediyor
Modeling and control of a fixed wing unmanned aerial vehicle
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2013
BURAK YÜKSEK
Gülay Öke Günel Tez Yüksek Lisans Tamamlandı
Coupling dynamic mesh technique and heuristic algorithms in 3 D tapered wing design
International Journal for Numerical Methods in Engineering, Vol. 74, No. 12, Haziran 2008, s. 1771-1794, ISSN: 00295981
VATANDAŞ OSMAN ERGÜVEN,OZKOL İBRAHİM
İbrahim Özkol Özgün Makale
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
Melike Nikbay Özgün Makale
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
Melike Nikbay Tam metin bildiri aeroelasticity
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
Melike Nikbay Tam metin bildiri Aeroelasticity
PIL simulations of an FWUAV under windy conditions
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 90, No. 2, 2018, s. 461-470, ISSN: 1748-8842
ÜLKER HAKAN,BAYKARA CEMAL,ÖZSOY İSMAİL CAN
Design of a flapping wing aerial vehicle based on four bar mechanism
2016 International Conference on Unmanned Aircraft Systems (ICUAS), Arlington, VA, USA/AMERİKA BİRLEŞİK DEVLETLERİ, 7 Haziran 2016
İŞBİTİRİCİ ABDURRAHMAN,ALTUĞ ERDİNÇ
Erdinç Altuğ Tam metin bildiri
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
The numerical simulation of the wing kinematic effects on near wake structure in hovering Drosophila flight,
Engineering Mechanics Institute Conference, 4 Haziran 2017
ERZINCANLI BELKIS,DILEK EZGI,ŞAHİN MEHMET
Mehmet Şahin Özet Bildiri
Mathematical model for takeoff simulation of a wing in proximity to the ground
Journal of Marine Science and Application, Vol. 15, 2016, s. 136-143
KINACI ÖMER KEMAL
Ömer Kemal Kınacı Özgün Makale
EFFECTS OF SPAN MORPHING ON FLUTTER CHARACTERISTICS OF SUBSONIC WING
14th World Congress on Computational Mechanics (WCCM) (ECCOMAS Congress 2020), 11 Ocak 2021
DURMUŞ DAMLA, KAYA METİN ORHAN
Metin Orhan Kaya Tam metin bildiri
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
Seher Eken Tam metin bildiri
Vibrational genetic algorithm VGA and dynamic mesh in the optimization of 3D wing geometries
Inverse Problems in Science and Engineering, Vol. 15, No. 6, Eylül 2007, s. 643-657, ISSN: 1741-5977
VATANDAŞ OSMAN ERGÜVEN,HACIOĞLU ABDURRAHMAN,OZKOL İBRAHİM
İbrahim Özkol Özgün Makale
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
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
İlker Murat Koç Tam metin bildiri
Large Scale Spanwise Periodic Vortex Gusts or Single Spanwise Vortex Impinging on a Rectangular Wing
2018 Fluid Dynamics Conference, Atlanta, Georgia/AMERİKA BİRLEŞİK DEVLETLERİ, 24 Haziran 2018
ENGİN KADER, AYDIN EGEMEN, ZALOĞLU BERK, FENERCİOĞLU AYDIN İDİL, ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN
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
Melike Nikbay Özgün Makale reliability
Cryptic diversity of the bent-wing bat, Miniopterus schreibersii (Chiroptera: Vespertilionidae), in Asia Minor
BMC EVOLUTIONARY BIOLOGY, Vol. 10, Ocak 2010, ISSN: 1471-2148
FURMAN ANDRZEJ,POSTAWA TOMASZ,OZTUNC TUNC,ÇORAMAN EMRAH
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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