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Özel Aralık Girişi

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
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
Sesaltı Bir Kanadın Pk Metodu ile Flutter Analizi
Kayseri VII. Havacılık Sempozyumu, KAYSERİ/TÜRKİYE, 15 Mayıs 2008
EKEN SEHER,ÖZDEMİR ÖZGE,ÖZÜNCER AYŞE DENİZ,KAYA METİN ORHAN
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 ÖZGE,KAYA METİN ORHAN
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
FLUTTER ANALYSIS AT TRANSONIC SPEEDS USING A COUPLED CFD-CSD SOLVER
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 18 Eylül 2019
ALPMAN EMRE,KAVURMACIOĞLU LEVENT ALİ,EKEN SEHER
Seher Eken Tam metin bildiri
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 AT TRANSONIC SPEEDS USING A COUPLED CFD-CSD SOLVER
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 18 Eylül 2019
ALPMAN EMRE,KAVURMACIOĞLU LEVENT ALİ,EKEN SEHER
Levent Ali Kavurmacıoğlu Tam metin bildiri
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 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
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
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
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
EFFECTS OF SPAN MORPHING ON FLUTTER CHARACTERISTICS OF SUBSONIC WING
14th World Congress on Computational Mechanics (WCCM) (ECCOMAS Congress 2020), 11 Ocak 2021
DURMUŞ DAMLA, KAYA METİN ORHAN
Metin Orhan Kaya Tam metin bildiri
Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover Part II
, Aircraft Engineering and Aerospace Technology: An International Journal, 2007
ÖZGE ÖZDEMİR ÖZGÜMÜŞ,KAYA METİN ORHAN
Metin Orhan Kaya Özgün Makale
The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Vol. 2, No. 2, 2015, s. 199-215, ISSN: 2287-528X
EKEN SEHER,KAYA METİN ORHAN
DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 20 Eylül 2017
CİHAN MELAHAT,EKEN SEHER,KAYA METİN ORHAN
Seher Eken Özet Bildiri
FORMULATION FOR FLUTTER AND VIBRATION ANALYSIS OF A HINGELESS HELICOPTER BLADE IN HOVER: PART I
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 2, Ocak 2007, s. 177-183, ISSN: 0002-2667
ÖZDEMİR ÖZGE,KAYA METİN ORHAN
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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