ARAMA SONUÇLARI

Toplam 30 adet sonuçtan 20 tanesi görüntülenmektedir.

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.

Burhaneddin Sandıkçı Özgün Makale Hospital bed capacity managementCare partitioningFocus

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

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

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

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

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

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

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

Seher Eken Özgün Makale limit cycle oscillationssweep angleharmonic balance methodNONLINEAR AEROELASTIC ANALYSISHOMOTOPY ANALYSIS METHODINCOMPRESSIBLE-FLOWRESTORING FORCESAIRFOIL MOTIONFLUTTERBIFURCATION

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

ARAMA SONUÇLARI

Arama

Yıllara göre arama