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MAİNİNİ LAURA,THELEN ANDREW,RUMPFKEİL MARKUS,QUAGLİARELLA DOMENİCO,FİORE FRANCESCO Dİ,SERANİ ANDREA,FİCİNİ SİMONE,PELLEGRİNİ RİCARDO,DİEZ MATTEO,MİNİSCİ EDMONDO,PEHLİVAN SOLAK HAYRİYE,YILDIZ ŞIHMEHMET,NİKBAY MELİKE,BRYSON DEAN,BERAN PHİLİP
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Chapter 5 Space Benchmark Definition” NATO STO-TR-AVT-331 Goal-Driven, Multi-Fidelity Approaches for Military Vehicle System-Level Design
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MİNİSCİ EDMONDO,LEYLAND PENELOPE,YILDIZ ŞIHMEHMET,NİKBAY MELİKE
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Chapter 9 Space Benchmark Results NATO STO-TR-AVT-331 Goal-Driven, Multi-Fidelity Approaches for Military Vehicle System-Level Design
2024, NATO Science and Technology Organization
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UNCERTAINTY QUANTIFICATION IN AEROELASTIC ANALYSES OF THE S4T WING USING REDUCED ORDER MODELING STO TR AVT 191 Application of Sensitivity Analysis and Uncertainty Qualification to Military Vehicle Design
Paris/FRANSA, 2017, s. 365-402, NATO Science and Technology Organization
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Comparison of Multi-Fidelity Optimization Methods Using an Aero-Structural Benchmark Problem
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BRYSON DEAN, BERAN PHİLİP, THELEN ANDREW, RUMPFKEİL MARKUS, NİKBAY MELİKE, ÇAKMAK ENES, YILDIZ ŞIHMEHMET
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Low Observable Uncrewed Aerial Vehicle Wind Tunnel Model Design, Manufacturing, and Aerodynamic Characterization
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ALEİSA HASSAN,KONTİS KONSTANTİNOS,NİKBAY MELİKE
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Reproducible industrial multi-fidelity optimization benchmark problems for air, space, and sea vehicles
NATO STO AVT-354 Multi-Fidelity Methods for Military Vehicle Design Workshop, Varna/BULGARİSTAN, 26 Eylül 2022
QUAGLİARELLA DOMENİCO, THELEN ANDREW, CLARK DANİEL, BRYSON DEAN, YILDIZ ŞIHMEHMET, NİKBAY MELİKE, MAİNİNİ LAURA, FİORE FRANCESCO Dİ, MİNİSCİ EDMONDO, LEYLAND PENELOPE, SERANİ ANDREA, FİCİNİ SİMONE, DİEZ MATTEO
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Integrating Analytical Aeroelastic Instability Analysis into Design Optimiza tion of Aircraft Wing Structures
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Design and implementation of a spread spectrum based communication system for an ingestible capsule
Proceedings of the Second Joint 24th Annual Conference and the Annual Fall Meeting of the Biomedical Engineering Society] [Engineering in Medicine and Biology, 23 Ekim 2002
AYDIN NİZAMETTİN,ARSLAN T,CUMMİNG DRS
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CONTROL OF AIR CONDITIONING WITH FUZZY LOGIC CONTROLLER DESIGN FOR SMART HOME SYSTEMS
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Design and Development of a New Tactile Stimulator
2019 NASA/ESA Conference on Adaptive Hardware and Systems (AHS), Colchester, United Kingdom/İNGİLTERE, 22 Temmuz 2019
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Aerodynamic Design Optimization of a Non-Planar C-Wing Configuration
10th Ankara International Aerospace Conference (AIAC), 18 Eylül 2019
SUKAS HULYA,PİRLEPELİ BERKAY,RAMESH KİRAN,NİKBAY MELİKE,KONTİS KONSTANTİNOS
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Robust Aeroelastic Design Optimization of Wing Store Configurations Based on Flutter Criteria
14th AIAA/ISSMO Multidisciplinary Analysis and Optimization (MAO) Conference, Indianapolis/AMERİKA BİRLEŞİK DEVLETLERİ, 17 Eylül 2012
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Aerostructural Design Optimization Of High Speed Wings For Reusable Launch Vehicles
10th Ankara International Aerospace Conference (AIAC), 18 Eylül 2019
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Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
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YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, NİKBAY MELİKE
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Reliability Based Design Optimization of a CubeSat De Orbiting Mechanism
14th AIAA/ISSMO Multidisciplinary Analysis and Optimization (MAO) Conference, Indianapolis/AMERİKA BİRLEŞİK DEVLETLERİ, 17 Eylül 2012
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Optimization of a plasma instrument design for a CubeSat with space weather research
7th International Conference on Recent Advances inSpace Technologies, Istanbul/TÜRKİYE, 16 Haziran 2015
NECMİ ORGER, YİGİT CAY, KAYMAZ ZEREFSAN, KARYOT BERAT, NİKBAY MELİKE
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Uncertainty Quantification of Aeroelastic Systems Using an Active Learning Gaussian Process
AeroBest 2021, An Eccomas Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, Lisbon (Virtual)/PORTEKİZ, 21 Temmuz 2021
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