ARAMA SONUÇLARI

Toplam 30 adet sonuçtan 20 tanesi görüntülenmektedir.

Boundary Moment Control of Free Vibration 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

Kaan Yıldız Tam metin bildiri

Approximate Analytical Solutions Of Nonlinear Flutter Of Aircraft Wings

IFASD 2011, 15th International Forum on Aeroelasticity and Structural Dynamics, Paris/FRANSA, 26 Haziran 2011

EKEN SEHER, KERKİ TİLBE, KAYA METİN ORHAN

Seher Eken Tam metin bildiri

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

Nuriye Leman Okşan Çetiner Yıldırım Tam metin bildiri

Limit Cycle Oscillations of Swept-back Wings In an Incompressible Flow

53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 23 Nisan 2012

EKEN SEHER, KAYA METİN ORHAN

Metin Orhan Kaya Tam metin bildiri

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

Active Vibration Control of Aircraft Wings Modeled as Thin-Walled Composite Beams Using Piezoelectric Actuation

ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers Digital Collection, MONTREAL/KANADA, 14 Kasım 2014

YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN

Kaan Yıldız Tam metin bildiri

Design and Control of a Mini Aerial Vehicle that has Four Flapping-Wings

Journal of Intelligent Robotic Systems, Vol. 88, No. 2-4, Mart 2017, s. 247-265, ISSN: 0921-0296

İŞBİTİRİCİ ABDURRAHMAN,ALTUĞ ERDİNÇ

Erdinç Altuğ Özgün Makale

Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams

AIAA-57th Structures, Structural Dynamics, and Materials Conference, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016

YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN

Seher Eken Tam metin bildiri

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

Aerostructural Design Optimization Of High Speed Wings For Reusable Launch Vehicles

10th Ankara International Aerospace Conference (AIAC), 18 Eylül 2019

CUSİCK ANDREW,KONTİS KONSTANTİNOS,NİKBAY MELİKE

Melike Nikbay Tam metin bildiri Launch VehicleOptimization

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