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Aerodynamic characteristics of external store configurations at low speeds
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Atomistic simulation of micro scale adiabatic piston problem
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SENGİL NEVSAN, EDİS FİRAT OGUZ
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Micro scale synthetic jet actuator flow simulation with characteristic based split method
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CELİK BAYRAM, EDİS FİRAT OGUZ
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Heuristic Algorithms for Aircraft Sequencing Problem
33rd International Annual Conference of the American Society for Engineering Management, VIRGINIA BEACH/AMERİKA BİRLEŞİK DEVLETLERİ, 17 Ekim 2012, s. 773-779
HANÇERLİOĞULLARI KÖKSALMIŞ GÜLŞAH, GHAITH RABADI, AMEER AL SALEM, KAHRBECHE MOHAMED
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Design and Development of a New Integrated Communication System for C-5 Galaxy Aircraft
Transactions of the SDPS. Journal of Integrated Design & Process Science, Vol. 2, No. 4, Mart 1999, s. 41-51, ISSN: 1092-0617
ÇİÇEK İSMAİL, SCHAFER DAVİD
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Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover Part II
, Aircraft Engineering and Aerospace Technology: An International Journal, 2007
ÖZGE ÖZDEMİR ÖZGÜMÜŞ,KAYA METİN ORHAN
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Optimization of the PD Coefficient in a Flight Simulator Control via Genetic Algorithms
Aircraft Engineering and Aerospace Technology: An International Journal, 2002
SAİT NURDOĞAN YURT,İBRAHİM ÖZKOL,KAYA METİN ORHAN,HACİYEV CHİNGİZ
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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, Vol. 798, Ekim 2015, s. 292-296, ISSN: 1662-7482
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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Solid rocket motor design using a surrogate model
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 90, No. 7, Ekim 2018, s. 1104-1127, ISSN: 1748-8842
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Integrating Analytical Aeroelastic Instability Analysis into Design Optimiza tion of Aircraft Wing Structures
TWMS Journal of Applied and Engineering Mathematics, Vol. 1, No. 2, 2011, s. 237-253
NİKBAY MELİKE,PİNAR ACAR
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Reliability Based Design Optimisation of an Aircraft Wing Structure with High Fidelity Modelling
International Journal of Design Engineering, Vol. 3, No. 3, 2011, s. 247-259
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Reliability Based Aeroelastic Optimization of a Com posite Aircraft Wing via Fluid Structure Interaction of High Fidelity Solvers
Materials Science and Engineering, Vol. 10, No. 1, 2010, s. 1-10
NİKBAY MELİKE,NECATİ FAKKUSOGLU,MUHAMMET NASİF KURU
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Multidisciplinary Code Coupling for Analysis and Optimization of Aeroelastic Systems
AIAA Journal of Aircraft, Vol. 46, No. 6, 2009, s. 1938-1944
NİKBAY MELİKE,LEVENT ONCU,AHMET AYSAN
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Reliability Based Multidisciplinary Optimization of Aeroelastic Systemswith Structural and Aerodynamic Uncertainties
AIAA Journal of Aircraft, Vol. 50, No. 3, 2013, s. 798-715, ISSN: 0021-8669
NİKBAY MELİKE,MUHAMMET NASİF KURU
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Reliability based aeroelastic optimization of a composite aircraft wing via fluid structure interaction of high fidelity solvers
IOP Conference Series: Materials Science and Engineering, Vol. 10, No. 1, Temmuz 2010, s. 12037, ISSN: 1757-899X
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Hovering Stability of a Model Helicopter
Aircraft Engineering and Aerospace Technology, Vol. 88, Ocak 2016, s. 810-817, ISSN: 1748-8842
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Greedy algorithms and metaheuristics for a multiple runway combined arrival departure aircraft sequencing problem
Journal of Air Transport Management, Vol. 32, Eylül 2013, s. 39-48, ISSN: 09696997
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Application of Weibull Distribution Method for Aircraft Component Life Estimation in Civil Aviation Sector
Journal of Traffic and Logistic Engineering, Temmuz 2017
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