Random Vibration of A Rectangular FGM Strip
3rd Aircraft Structural Design Conference, 9 Ekim 2012
DOĞAN VEDAT ZİYA
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Dynamic Finite Element Analysis of an Aircraft Seat
7th Ankara International Aerospace Conference, 11 Eylül 2013
DOĞAN VEDAT ZİYA,SİMİTCİOĞLU GÖKAY
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Approximate Algorithms for Aircraft Rescheduling Problems Under Operation Disruptions
2012 INFORMS Annual Meeting, PHOENIX/AMERİKA BİRLEŞİK DEVLETLERİ, 14 Ekim 2012
HANÇERLİOĞULLARI KÖKSALMIŞ GÜLŞAH, RABADI GHAITH
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Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
Algorithms, Temmuz 2022, ISSN: 1999-4893
YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, NİKBAY MELİKE
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Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
Journal of Aircraft, Mart 2023, ISSN: 1533-3868
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF, NİKBAY MELİKE
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Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design
AIAA Scitech 2021 Forum, 11 Ocak 2021
DEMİROĞLU YUSUF, YILDIZ ŞIHMEHMET, NİKBAY MELİKE
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Decentralized optimization with application to multiple aircraft coordination
41st IEEE Conference on Decision and Control, 10 Aralık 2002
İNALHAN GÖKHAN,STİPANOVİC DUSAN,TOMLİN CLAİRE
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Scheduled Maintenance and Downtime Cost in Aircraft Maintenance Management
International Journal of Mechanical, Aerospace, Industrial, Mechatronic and Manufacturing Engineering, Haziran 2016
SALTOĞLU REMZİ,HUMAİRA NAZMİA,İNALHAN GÖKHAN
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Aircraft Scheduled Airframe Maintenance and Downtime Integrated Cost Model
ADVANCES IN OPERATIONS RESEARCH, Haziran 2016
SALTOĞLU REMZİ,HUMAİRA NAZMİA,İNALHAN GÖKHAN
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Autonomous Execution of Aircraft Supermaneuvers with Switching Nonlinear Backstepping Control
AIAA Scitech, 8 Ocak 2018
MOGHADAM MAJİD,ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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Recoverability Envelope Analysis of Nonlinear Control Laws for Agile Maneuvering Aircraft
AIAA Scitech, 8 Ocak 2018
AKÇAL UĞUR,HOŞTAŞ BATUHAN,ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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Hovering Stability of a Model Helicopter
Aircraft Engineering and Aerospace Technology, Ocak 2015
KOÇ İLKER MURAT,FRANKO SAMUEL,ÖZSOY İSMAİL CAN
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TOPOLOGY OPTIMIZATION AND STRUCTURAL ANALYSIS AN AIRCRAFT WING
10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 18 Eylül 2019
İNCİ HARUN, ÇAMUR ZELİHA, EKEN SEHER
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Aeroelastic Analysis of a Tapered Aircraft Wing
4th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 10 Eylül 2007
EKEN SEHER, ÖZDEMİR ÖZGE, KAYA METİN ORHAN
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Aeroelastic instability of aircraft wings modeled as thin-walled composite beams
7th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 11 Eylül 2013
EKEN SEHER, KAYA METİN ORHAN
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Free Vibration Analysis of Rotating Timoshenko Beam by Differential Transform Metho
Aircraft Engineering and Aerospace Technology: An International Journal, 2006
KAYA METİN ORHAN
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Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin Walled Composite Beams
Applied Mechanics and Materials, Ekim 2015
KAAN YILDIZ,SEHER EKEN,KAYA METİN ORHAN
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Using the Dynamic Mesh Method for Genetically Obtained Wing Structures
Aircraft Engineering and Aerospace Technology: An International Journal, 2004
ERGÜVEN VATANDAS,İBRAHİM ÖZKOL,KAYA METİN ORHAN
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Vibration Analysis of a Hingeless helicopter blade in hover Part I
Aircraft Engineering and Aerospace Technology: An International Journal, 2007
ÖZGE ÖZDEMİR ÖZGÜMÜŞ,KAYA METİN ORHAN
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Learning-based Aircraft Trajectory Planning Enhancement
AIAA Scitech 2019 Forum, San Diego/AMERİKA BİRLEŞİK DEVLETLERİ, 7 Ocak 2019
ALİZADEH ALİ,HUMAİRA NAZMİA,KOYUNCU EMRE
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