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Özel Aralık Girişi

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
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
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
Melike Nikbay Tam metin bildiri FlutterRoket
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
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
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
Zahit Mecitoğlu Özgün Makale
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
Seher Eken Özet Bildiri
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
Seher Eken Tam metin bildiri
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
Investigation of the effect of different modal analysis methods on flutter speed calculation
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2020
BİLGEHAN ŞEREF
Vedat Ziya Doğan Tez Yüksek Lisans Tamamlandı
Vibration and flutter analysis of fluid loaded plates
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1996
ABDURRAHMAN ŞEREF CAN
Zahit Mecitoğlu Tez Yüksek Lisans Tamamlandı
FLUTTER ANALYSIS OF GOLAND WING VIA FINITE ELEMENT METHOD
6. ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 14 Eylül 2011
ÖZDEMİR ÖZGE, EKEN SEHER, KAYA METİN ORHAN
Metin Orhan Kaya Tam metin bildiri
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
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
Levent Ali Kavurmacıoğlu Tam metin bildiri
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
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
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
Seher Eken 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
A numerical method for the dynamic stability analysis of supported plates in open and confined axial flow
OCEAN ENGINEERING, Vol. 258, Ocak 2022, ISSN: 0029-8018
UĞURLU BAHADIR, TUNCA ENES, KAHRAMAN İSMAİL
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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