Flutter and Vibration of A Hingeless Helicopter Blade in Hover
3rd Ankara International Aerospace Conference, ANKARA/TÜRKİYE, 22 Ağustos 2005
KAYA METİN ORHAN, ÖZDEMİR ÖZGE
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Sesaltı Bir Kanadın Pk Metodu ile Flutter Analizi
Kayseri VII. Havacılık Sempozyumu, KAYSERİ/TÜRKİYE, 15 Mayıs 2008
DURMAZ SEHER, ÖZDEMİR ÖZGÜMÜŞ ÖZGE, ÖZÜNCER AYŞE DENİZ, KAYA METİN ORHAN
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Investigation of the Effect of Thickness Taper Ratio and Aspect Ratio on Fin Flutter Velocity of a Model Rocket using Response Surface Method
7th International Conferenceon Recent Advances in Space Technologies, Istanbul/TÜRKİYE, 16 Haziran 2015
CEYHUN TOLA,NİKBAY MELİKE
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Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: part II. Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 3, Mayıs 2007, s. 231-237, ISSN: 0002-2667
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
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Flutter of a Membrane in a Stagnation Flow
JOURNAL OF APPLIED FLUID MECHANICS, Vol. 12, No. 3, Mayıs 2019, s. 981-985, ISSN: 1735-3572
KAPKİN ŞULE,DEMİR MEHMET ŞİRİN,KAYA METİN ORHAN,UZAL EROL
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Flutter Analysis of A Laminated Composite Plate wit Temperature Dependent Material Properties
International Journal of Aeronautical Science and Aerospace Research, Haziran 2016
KAZANCI ZAFER,MECİTOĞLU ZAHİT
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Flutter Analysis Of Goland Wing Via Finite Element Method
6th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 14 Eylül 2011
ÖZDEMİR ÖZGE, EKEN SEHER, KAYA METİN ORHAN
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FLUTTER ANALYSIS AT TRANSONIC SPEEDS USING A COUPLED CFD-CSD SOLVER
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 18 Eylül 2019
ALPMAN EMRE, KAVURMACIOĞLU LEVENT ALİ, EKEN SEHER
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Flutter analysis of wing/store configurations with applications to robust aeroelastic optimization
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2012
PINAR ACAR
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Investigation of the effect of different modal analysis methods on flutter speed calculation
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
BİLGEHAN ŞEREF
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Vibration and flutter analysis of fluid loaded plates
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1996
ABDURRAHMAN ŞEREF CAN
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FLUTTER ANALYSIS OF GOLAND WING VIA FINITE ELEMENT METHOD
6. ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 14 Eylül 2011
ÖZDEMİR ÖZGE, EKEN SEHER, KAYA METİN ORHAN
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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
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FLUTTER ANALYSIS AT TRANSONIC SPEEDS USING A COUPLED CFD-CSD SOLVER
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 18 Eylül 2019
ALPMAN EMRE, KAVURMACIOĞLU LEVENT ALİ, EKEN SEHER
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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
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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
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Sesaltı bir Kanadın p-k Metodu ile Flutter Analizi
VII. Havacılık Sempozyumu, Kayseri/TÜRKİYE, 15 Mayıs 2008
EKEN SEHER, ÖZDEMİR ÖZGE, OZUNCER AYSE DENİZ, 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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The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Vol. 2, No. 2, Ocak 2015, s. 199-215, ISSN: 2287-528X
EKEN SEHER, KAYA METİN ORHAN
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DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 20 Eylül 2017
CİHAN MELAHAT, EKEN SEHER, KAYA METİN ORHAN
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