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Özel Aralık Girişi

Force Measurement and Load Estimation Studies at ITU forFlexible Flapping Wings and Maneuvering Wings under Gust
International Workshop on Non-Intrusive Optical Flow Diagnostics, 25 Ekim 2016
SON ONUR,ZALOĞLU BERK,PERÇİN MUSTAFA,ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN
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
The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Nisan 2015
SEHER EKEN,KAYA METİN ORHAN
Metin Orhan Kaya Özgün Makale
Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin Walled Composite Beams
Applied Mechanics and Materials, Ekim 2015
KAAN YILDIZ,SEHER EKEN,KAYA METİN ORHAN
Metin Orhan Kaya Özgün Makale
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
Investigation of flow field around flapping wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2007
KEREM ANBARCI
Fırat Oğuz Edis 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
Dynamic analysis of adaptive aircraft wings modelled as thin-walled composite beams
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2015
KAAN YILDIZ
Metin Orhan Kaya Tez Yüksek Lisans Tamamlandı
Design and Control of a Mini Aerial Vehicle that has Four Flapping-Wings
Journal of Intelligent Robotic Systems, Vol. 88, No. 2-4, Mart 2017, s. 247-265, ISSN: 0921-0296
İŞBİTİRİCİ ABDURRAHMAN,ALTUĞ ERDİNÇ
Erdinç Altuğ Özgün Makale
Limit Cycle Oscillations of Swept-back Wings In an Incompressible Flow
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 23 Nisan 2012
EKEN SEHER, KAYA METİN ORHAN
Metin Orhan Kaya Tam metin bildiri
Managing Hospital Inpatient Bed Capacity Through Partitioning Care into Focused Wings
Manufacturing & Service Operations Management, Vol. 17, No. 2, Nisan 2015, s. 157-176, ISSN: 1523-4614","1526-5498
BEST THOMAS J., SANDIKÇI BURHANEDDİN, EİSENSTEİN DONALD D., MELTZER DAVİD O.
Performance Prediction of Wings Moving Above Free Surface
Advances in Boundary Element and Meshless Techniques XVII, Ankara/TÜRKİYE, 11 Temmuz 2016, s. 85-92
DOĞRUL ALİ,BAL ŞAKİR
Şakir Bal Tam metin bildiri
Aerostructural Design Optimization Of High Speed Wings For Reusable Launch Vehicles
10th Ankara International Aerospace Conference (AIAC), 18 Eylül 2019
CUSİCK ANDREW,KONTİS KONSTANTİNOS,NİKBAY MELİKE
Active Vibration Control of Aircraft Wings Modeled as Thin-Walled Composite Beams Using Piezoelectric Actuation
ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers Digital Collection, MONTREAL/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Kaan Yıldız Tam metin bildiri
Boundary Moment Control of Free Vibration of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
8th Ankara International Aerospace Conference, ANKARA/TÜRKİYE, 10 Eylül 2015
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Kaan Yıldız Tam metin bildiri
Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, California, USA/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN,EKEN SEHER,KAYA METİN ORHAN
Kaan Yıldız Tam metin bildiri
Approximate Analytical Solutions Of Nonlinear Flutter Of Aircraft Wings
IFASD 2011, 15th International Forum on Aeroelasticity and Structural Dynamics, Paris/FRANSA, 26 Haziran 2011
EKEN SEHER, KERKİ TİLBE, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Active vibration control of aircraft wings modeled as thin-walled composite beams using piezoelectric actuation
ASME-IMECE-2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
AIAA-57th Structures, Structural Dynamics, and Materials Conference, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Limit Cycle Oscillations Of Swept-Back Wings in an incompressible Flow
AIAA-53rd Structures, Structural Dynamics, and Materials Conference, Honolulu-Hawaii/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Nisan 2012
EKEN SEHER, KAYA METİN ORHAN
Seher Eken Tam metin bildiri

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