Vibration response analysis of an aircraft structure in terms of crashworthiness by using differential transformation method
Gazi University Journal of Science, Vol. 37, Aralık 2024, ISSN: 2147-1762
SOYSAL AYSUN,ÖZKOL İBRAHİM,UZAL EROL
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Mission Planning and Control of Multi-Aircraft Systems With Signal Temporal Logic Specifications
IEEE Access, Vol. 7, Ekim 2019, s. 155941-155950, ISSN: 2169-3536
BAŞPINAR BARIŞ, BALAKRİSHNAN HAMSA, KOYUNCU EMRE
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Meta Heuristics for Aircraft Arrival and Departure Scheduling on Multiple Runways
IIE Annual Conference and Expo 2012, ORLANDO/AMERİKA BİRLEŞİK DEVLETLERİ, 19 Mayıs 2012, s. 1235-1242
RABADI GHAITH, HANÇERLİOĞULLARI KÖKSALMIŞ GÜLŞAH, KHARBECHE MOHAMED, ALSALEM AMEER
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Aeroelastic Analysis of A Tapered Aircraft Wing
4th Ankara International Aerospace Conference, ANKARA/TÜRKİYE, 10 Eylül 2007
SEHER DURMAZ, ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
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Design and Optimization of Generator for Narrow Body Commercial Aircraft
11th INTERNATIONAL CONFERENCE onELECTRICAL and ELECTRONICS ENGINEERING, Bursa/TÜRKİYE, 28 Kasım 2019, s. 1007-1011
TAŞKIN MEHMET MURATHAN,CANSIZ AHMET
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Boundary Moment Control of Free Vibration 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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Devulcanized rubber based composite design reinforced with nano silica, graphene nano platelets (GnPs) and epoxy for “aircraft wing spar” to withstand bending moment
Annual Conference Society for Experimental Mechanics 2018, 4 Haziran 2018, s. 9, ISSN: 21915652 21915644
İREZ ALAEDDİN BURAK,BAYRAKTAR EMİN,MİSKİOGLU İBRAHİM
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Design of a flapping wing aerial vehicle based on four bar mechanism
2016 International Conference on Unmanned Aircraft Systems (ICUAS), Arlington, VA, USA/AMERİKA BİRLEŞİK DEVLETLERİ, 7 Haziran 2016
İŞBİTİRİCİ ABDURRAHMAN,ALTUĞ ERDİNÇ
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Optimization of Aircraft Utilization by Reducing Scheduled Maintenance Downtime
10th Annual AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, FORT WORTH/AMERİKA BİRLEŞİK DEVLETLERİ, 13 Eylül 2010
ŞENTÜRK CANER, KAVSAOĞLU MEHMET, 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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A Low Cost Prototyping Approach for Design Analysis and Flight Testing of the TURAC VTOL UAV
2014 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS), 27 Mayıs 2014
İNALHAN GÖKHAN, VURUŞKAN ASLIHAN, DERELİ YASİN, KAYA METİN ORHAN
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Inverse solutions of the Prandtl Meyer function
Journal of Aircraft, Vol. 31, No. 6, Kasım 1994, s. 1422-1424, ISSN: 0021-8669
ÖZCAN OKTAY,EDİS FIRAT OĞUZ,ASLAN ALİM RÜSTEM,PINAR I
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Finite State Automata Based Approach to Autonomous Stall and Upset Recovery for Agile Aircraft
AIAA Scitech, 8 Ocak 2018
YILDIZ ANIL,AKÇAL UĞUR,HOŞTAŞ BATUHAN,ÜRE NAZIM KEMAL,İNALHAN GÖKHAN
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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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Analysis of NO NO2 and O3 Between Model Simulations and Ground Based Aircraft and Satellite Observations
Water, Air, & Soil Pollution, Vol. 224, No. 9, Eylül 2013, ISSN: 0049-6979
KAYNAK BURÇAK,HU YONGTAO,RUSSELL ARMİSTEAD G
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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
KOÇ İLKER MURAT,SEMUEL FRANKO,ÖZSOY İSMAİL CAN
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Data-Driven Trajectory Uncertainty Quantification For Climbing Aircraft To Improve Ground-Based Trajectory Prediction
ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering, Vol. 18, No. 2, Haziran 2017, s. 323-345, ISSN: 1302-3160
UZUN MEVLÜT, KOYUNCU EMRE
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Multi-objective and Gradient Based Structural Design Optimization of an Aircraft Wing
ASMDO Second International Conference on Multidisciplinary Design Optimization and Applications, 2 Eylül 2008
NİKBAY MELİKE,YANANGONUL ARDA,ONCU LEVENT,KOCAS MURAT
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The effects of the use of single task-oriented maintenance concept and more accurate letter check alternatives on the reduction of scheduled maintenance downtime of aircraft
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
SENTURK CANER,OZKOL İBRAHİM
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Dynamic mesh and heuristic algorithms for the design of a transonic wing
Aircraft Engineering and Aerospace Technology, Vol. 78, No. 1, Ocak 2006, s. 39-44, ISSN: 0002-2667
VATANDAŞ OSMAN ERGÜVEN,OZKOL İBRAHİM
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