Vibration of anti symmetric angle ply composite plates under random excitation
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 5, Eylül 2007, s. 475-484, ISSN: 0002-2667
DOĞAN VEDAT ZİYA
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Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
MDPI Algorithms, Vol. 15, No. 7, Temmuz 2022, ISSN: 1999-4893
YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, NİKBAY MELİKE
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Boundary Moment Control of Free Vıbratıon 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
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Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, San Diego, California, USA/AMERİKA BİRLEŞİK DEVLETLERİ, 4 Ocak 2016
YILDIZ KAAN,EKEN SEHER,KAYA METİN ORHAN
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A DEPLOYMENT OF FILM COOLING HOLES ON A SQUEALER TURBINE BLADE TIP
International Symposium on Aircraft Technology, MRO Operations, 25 Kasım 2018
YILDIZ FARUK,ALPMAN EMRE,KAVURMACIOĞLU LEVENT ALİ
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F-16 JET AIRCRAFT EXPLICIT MODEL FOLLOWING BASED LONGITUDINAL CONTROLLER DESIGN AND ANGLE OF ATTACK ESTIMATION
GSRD International Conference, İstanbul/TÜRKİYE, 21 Aralık 2022
KESGİN ERTÜRK GÜLŞAH, ÜSTOĞLU İLKER
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Secure Communication for MUM-T: A Blockchain and Lightweight Cryptography Framework
2024 17th International Conference on Security of Information and Networks (SIN), Sydney/AVUSTRALYA, 2 Aralık 2024, s. 1-8
YAŞAR HALİMCAN,BAHTİYAR ŞERİF
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Sugeno and Mamdani based Fuzzy Inference Approaches for Aircraft Pitch Control
International Conference on Mathematics and Mathematics Education (ICMME), URFA/TÜRKİYE, 11 Mayıs 2017
ÖZTÜRK MUHAMMET,BAYEZİT İSMAİL,OKUDAN MEHMET EMİN,OZKOL İBRAHİM
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Active vibration control of aircraft wings modeled as thin-walled composite beams using piezoelectric actuation
ASME-IMECE-2014, International Mechanical Engineering Congress & Exposition, Montreal/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
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Design and Analysis of a High Power Density Brushless DC Motor for a Multi-Rotor Unmanned Aircraft
13th International Conference on Electrical and Electronics Engineering (ELECO 2021), Bursa/TÜRKİYE, 25 Kasım 2021
OZER KEVSER, YILMAZ MURAT
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Multi-Fidelity and Multi-Disciplinary Design Optimization of A Low-Boom Supersonic Transport Aircraft
2023 AIAA Scitech Forum, National Harbor, Maryland/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Ocak 2023
NİKBAY MELİKE, KILIÇ DİLAN, ÇAKMAK ENES, TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF
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Free vibration analysis of a rotating double tapered beam with flexible root via differential quadrature method
Aircraft Engineering and Aerospace Technology, Vol. 93, Ocak 2021, ISSN: 1748-8842
OZKOL İBRAHİM, YAVUZ MUSTAFA TOLGA
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Dynamic Stall Alleviation using a Deformable Leading Edge Concept A Numerical Study
JOURNAL OF AIRCRAFT, Vol. 40, 2003, s. 77-85, ISSN: 0021-8669
ŞAHİN MEHMET,LAKSHIMI SANKAR,CHANDRASEKHARA MUGURU,TUNG CHEE
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The stability dependence on the different pressure gradients in a channel flow
Aircraft Engineering and Aerospace Technology, Vol. 75, No. 5, Ekim 2003, s. 485-490, ISSN: 0002-2667
SÖYLEMEZ HARUN TAYFUN,OZKOL İBRAHİM
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AEROELASTIC RESPONSE OF AN AIRCRAFT WING MODELED AS A THIN-WALLED COMPOSITE BEAM
ASME-IMECE2013, International Mechanical Engineering Congress & Exposition, San Diego-California/AMERİKA BİRLEŞİK DEVLETLERİ, 14 Kasım 2013
EKEN SEHER, KAYA METİN ORHAN
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Development of A Sonic Boom Propagation Code For Low-Boom Supersonic Aircraft Design and Optimization
AIAA SCITECH 2023 Forum, National Harbor, Maryland/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Ocak 2023
DEMİROGLU YUSUF, NİKBAY MELİKE
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Ses-Ustu Bir Ucak Modelinin Govdesi icin Sonik Patlama Op- timizasyonu (Sonic Boom Minimization of a Supersonic Aircraft Fuselage)
8. Ulusal Havacilik ve Uzay Konferansi, Ankara/TÜRKİYE, 9 Eylül 2020
YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF, NİKBAY MELİKE
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Effects of Various Baffle Designs on Center Of Gravity Deviation in a Training Aircraft Wing Fuel Tank Using 1D Simulations
Proceedings of the ASME 2023 International Mechanical Engineering Congress and Exposition (IMECE2023), New Orleans/AMERİKA BİRLEŞİK DEVLETLERİ, 29 Ekim 2023
KARAHAN KEREM, ÇADIRCI SERTAÇ
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Sugeno and Mamdani based Fuzzy Inference Approaches for Aircraft Pitch Control
International Conference on Mathematics and Mathematics Education (ICMME), URFA/TÜRKİYE, 11 Mayıs 2017
ÖZTÜRK MUHAMMET,BAYEZİT İSMAİL,OKUDAN MEHMET EMİN,OZKOL İBRAHİM
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Applications of Metal Additive Manufacturing in Aircraft Components
1st International Conference on Smart Innovation in Science and Engineering, Salalah/UMMAN, 7 Nisan 2021, s. 30-31
YILDIZ RAŞİD AHMED
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