Performance Prediction of Wings Moving Above Free Surface
Advances in Boundary Element and Meshless Techniques XVII, Ankara/TÜRKİYE, 11 Temmuz 2016, s. 85-92
DOĞRUL ALİ,BAL ŞAKİR
|
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 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
|
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
|
Managing Hospital Inpatient Bed Capacity Through Partitioning Care into Focused Wings
Manufacturing & Service Operations Management, Vol. 17, No. 2, Nisan 2015, s. 157-176, ISSN: 1523-4614","1526-5498
BEST THOMAS J., SANDIKÇI BURHANEDDİN, EİSENSTEİN DONALD D., MELTZER DAVİD O.
|
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
|
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
|
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
|
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
|
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
|
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
|
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
|
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
|
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
|