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Özel Aralık Girişi

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
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
Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 2, Şubat 2007, s. 177-183, ISSN: 0002-2667
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
EFFECTS OF SPAN MORPHING ON FLUTTER CHARACTERISTICS OF SUBSONIC WING
14th World Congress on Computational Mechanics (WCCM) ECCOMAS Congress 2020) Virtual Congress: 11-–15 January 2021, 11 Ocak 2021
DURMUŞ DAMLA, KAYA METİN ORHAN
Metin Orhan Kaya Tam metin bildiri

İLETİŞİM BİLGİLERİ

İstanbul Teknik Üniversitesi Rektörlüğü İTÜ Ayazağa Kampüsü Rektörlük Binası, Maslak-Sarıyer / İstanbul Tel: +90 212 285 3930