ARAMA SONUÇLARI

Toplam 26 adet sonuçtan 20 tanesi görüntülenmektedir.

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

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

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

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