ARAMA SONUÇLARI

Toplam 30 adet sonuçtan 20 tanesi görüntülenmektedir.

Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams

Applied Mechanics and Materials, Vol. 798, Ocak 2015, s. 292-296, ISSN: 1660-9336

YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN

Seher Eken Özgün Makale

Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections

Thin-Walled Structures, Vol. 139, Haziran 2019, s. 362-371, ISSN: 0263-8231

EKEN SEHER

Seher Eken Özgün Makale

Flexural-torsional coupled vibration of anisotropic thin-walled beams with biconvex cross-section

THIN-WALLED STRUCTURES, Vol. 94, Ocak 2015, s. 372-383, ISSN: 0263-8231

EKEN SEHER, KAYA METİN ORHAN

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

Boundary Moment Control of Free Vıbratıon of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams

8th Ankara International Aerospace Conference, ankara/TÜRKİYE, 10 Eylül 2015

YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN

Seher Eken Tam metin bildiri

Introduction to the Virtual Collection: Unsteady Aerodynamic Response of Rigid Wings in Large-Amplitude Gust Encounters

AIAA JOURNAL, Vol. 59, No. 3, Mart 2021, s. 764-764, ISSN: 1748-717X

JONES ANYA R., ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN

Overview of Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters

AIAA JOURNAL, Vol. 59, No. 2, Şubat 2021, s. 731-736, ISSN: 1748-717X

JONES ANYA R., ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN

Overview of NATO AVT-282: Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters

AIAA Scitech 2020 Forum, Orlando, Florida/AMERİKA BİRLEŞİK DEVLETLERİ, 6 Ocak 2020

JONES ANYA R., ÇETİNER YILDIRIM NURİYE LEMAN OKŞAN

Free Surface Effects on 2 D Airfoils and 3 D Wings Moving Over Water

Ocean Systems Engineering, An International Journal, Vol. 6, No. 3, Eylül 2016, s. 245-264

BAL ŞAKİR

Şakir Bal Özgün Makale

Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams

Applied Mechanics and Materials, Vol. 798, Ekim 2015, s. 292-296, ISSN: 1662-7482

YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN

Kaan Yıldız Özgün Makale