ARAMA SONUÇLARI

Toplam 42 adet sonuçtan 20 tanesi görüntülenmektedir.

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Özel Aralık Girişi

A Multi-fidelity Aerodynamic Surrogate Model Implementation for Aeroelastic Optimization of a Nonplanar Lifting Surface
AeroBest 2021, An Eccomas Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, Lisbon (Virtual)/PORTEKİZ, 21 Temmuz 2021
PİRLEPELİ BERKAY, NİKBAY MELİKE, KONTİS KONSTANTİNOS
Aeroelastic Uncertainty Quantification Studies Using the S4T Wind Tunnel Model
AIAA Scitech, Dallas/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ocak 2017
NİKBAY MELİKE,HEEG JENNİFER
Aeroelastic Analysis of a Tapered Aircraft Wing
4th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 10 Eylül 2007
EKEN SEHER, ÖZDEMİR ÖZGE, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Aeroelastic instability of aircraft wings modeled as thin-walled composite beams
7th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 11 Eylül 2013
EKEN SEHER, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Steady-state aeroelastic analysis and numerical design optimization of aircraft structures
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2009
ARDA YANANGÖNÜL
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Structural identification and static aeroelastic optimization of ARW-2 wing with multidisciplinary code coupling
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2009
AHMET AYSAN
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Reliability based structural and aeroelastic optimization of wing models with high fidelity solvers
Bilişim Enstitüsü, İstanbul Teknik Üniversitesi, 2011
MUHAMMET NASIF KURU
Melike Nikbay Tez Yüksek Lisans Tamamlandı
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
Multidisciplinary design optimization of aerospace structures with static aeroelastic criteria
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2008
LEVENT ÖNCÜ
Melike Nikbay Tez Yüksek Lisans Tamamlandı
Dynamic and aeroelastic analysis of a wind turbine blade modeled as a thin-walled composite beam
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2018
SERHAT YILMAZ
Metin Orhan Kaya Tez Doktora Tamamlandı
Dynamic and aeroelastic analysis of advanced aircraft wings carrying external stores
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
ALEV KAÇAR AKSONGUR
Metin Orhan Kaya Tez Doktora Tamamlandı
Dynamic and aeroelastic analysis of a helicopter blade with actively controlled trailing edge flap in forward flight
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2012
ÖZGE ÖZDEMİR ÖZGÜMÜŞ
Metin Orhan Kaya Tez Doktora Tamamlandı
Aeroelastic analysis of variable-span morphing wing
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
DAMLA DURMUŞ
Metin Orhan Kaya Tez Yüksek Lisans Tamamlandı
Nonlinear dynamic and aeroelastic analyses of aircraft wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2013
SEHER DURMAZ
Metin Orhan Kaya Tez Doktora Tamamlandı
Aeroelastic analysis of 2 dof typical airfoil section modeled with shape memory alloy springs
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
OSMAN DAĞLI
Metin Orhan Kaya Tez Yüksek Lisans Tamamlandı
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
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
Euler Solver Based Aeroelastic Predictions for Steady and UnsteadyFlow Characteristics of HIRENASD Wing NATO STO AVT 203 Joined Exercise on Aeroelastic Prediction
Paris/FRANSA, 2017, s. 131-150, NATO Science and Technology Organization
NİKBAY MELİKE,PİNAR ACAR,ZANG ZHİCHAO
Melike Nikbay Bilimsel KitapKitap Bölümü
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
Impact of Aeroelastic Uncertainties on Sonic Boom Signature of a Commercial Supersonic Transport Configuration
AIAA Scitech Forum, Dallas/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ocak 2017
NİKBAY MELİKE,STANFORD BRET,WEST TOM,RALLABHANDİ SRİRAM

İLETİŞİM BİLGİLERİ

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