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
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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
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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
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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
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Dynamic and aeroelastic analysis of advanced aircraft wings carrying external stores
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
ALEV KAÇAR AKSONGUR
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Investigation of flow field around flapping wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2007
KEREM ANBARCI
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Nonlinear dynamic and aeroelastic analyses of aircraft wings
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2013
SEHER DURMAZ
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Dynamic analysis of adaptive aircraft wings modelled as thin-walled composite beams
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2015
KAAN YILDIZ
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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
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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
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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.
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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
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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
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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
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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
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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
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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
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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
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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
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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
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