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Özel Aralık Girişi

Flutter analysis of wing/store configurations with applications to robust aeroelastic optimization
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2012
PINAR ACAR
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Analytical study of a flapping wing of an unmanned air vehicle and testing of the prototype
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2010
EVREN KIRAN
Fırat Oğuz Edis Tez Yüksek Lisans Tamamlandı
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
Melike Nikbay Tam metin bildiri
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
Melike Nikbay Tam metin bildiri
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
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
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
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
The Numerical Simulation of the Wing Kinematic Effects on Near Wake Structure and Aerodynamic Performance in Hovering Drosophila Flight
COMPUTER AND FLUIDS, Vol. 122, Kasım 2015, s. 90-110
BELKİS ERZİNCANLİ,ŞAHİN MEHMET
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
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
Finite Element Analysis of a Thin Walled Composite Wing by Including Warping Effects
ASME International Mechanical Engineering Congress and Exposition, VANCOUVER/KANADA, Vol. 13, 12 Kasım 2010
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, DURMAZ SEHER, KAYA METİN ORHAN
Flutter Analysis of Goland Wing via Finite Element Method
6th Ankara International Aerospace Conference, ANKARA/TÜRKİYE, 14 Eylül 2011
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, EKEN SEHER, KAYA METİN ORHAN
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
An iterative boundary element method for a wing in ground effect
International Journal of Naval Architecture and Ocean Engineering, Vol. 6, No. 2, Haziran 2014, s. 282-296, ISSN: 2092-6782
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
Immersion and invariance control for Euler angles of a fixed-wing unmanned aerial vehicle
Asian Journal of Control, Vol. 24, No. 4, Temmuz 2022, s. 1585-1596, ISSN: 1561-8625
ASLAN FIRAT, YALÇIN YAPRAK
Yaprak Yalçın Özgün Makale Control
Numerical and experimental modal analyses of inclined supported bridge wing structures
INTERNATIONAL JOURNAL OF ACOUSTICS AND VIBRATION, Vol. 27, No. 1, Mart 2022, s. 56-66, ISSN: 1027-5851
YÜCEL ADİL
Adil Yücel Özgün Makale
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
Seher Eken Tam metin bildiri

İLETİŞİM BİLGİLERİ

İstanbul Teknik Üniversitesi Rektörlüğü İTÜ Ayazağa Kampüsü Rektörlük Binası, Maslak-Sarıyer / İstanbul Tel: +90 212 285 3930