ARAMA SONUÇLARI

Toplam 26 adet sonuçtan 20 tanesi görüntülenmektedir.

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

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

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

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) Virtual Congress: 11-–15 January 2021, 11 Ocak 2021

DURMUŞ DAMLA, KAYA METİN ORHAN

Metin Orhan Kaya Tam metin bildiri