The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Nisan 2015
SEHER EKEN,KAYA METİN ORHAN
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Image Based and Hybrid Visual Servo Control of an Unmanned Aerial Vehicle Recent Developments in Unmanned Aircraft Systems
2012, Springer
ZEHRA CEREN,ALTUĞ ERDİNÇ
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Kalman filter and neural network based icing a identification applied to A340 aircraft dynamics
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Ocak 2005, ISSN: 0002-2667
AYKAN RAHMİ,HACIZADE CENGİZ,ÇALIŞKAN FİKRET
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Local thermal non-equilibrium conjugate forced convection and entropy generation in an aircraft cabin with air channel partially filled porous insulation
Aircraft Engineering and Aerospace Technology, Kasım 2021, ISSN: 1748-8842
ÇİÇEK OKTAY, BAYTAŞ AHMET CİHAT
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Cooperative Terrain-Based GNSS-Denied Navigation With Particle Filter
IEEE ACCESS, Vol. 13, Ocak 2025, s. 11, ISSN: 2169-3536
YENGİN ZİYA UYGAR,KOYUNCU EMRE
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The effect of sweep angle on the limit cycle oscillations of aircraft wings
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Vol. 2, No. 2, Ocak 2015, s. 199-215, ISSN: 2287-528X
EKEN SEHER, KAYA METİN ORHAN
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Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 2, Şubat 2007, s. 177-183, ISSN: 0002-2667
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
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Investigation of Nacelle Design Parameters for a Supersonic Aircraft with Low Fidelity Approaches
11th Ankara International Aerospace Conference (AIAC), Ankara (Virtual)/TÜRKİYE, 8 Eylül 2021
OMER OZYILMAZ, NİKBAY MELİKE
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270VDC Power Architecture for More Electric Aircraft: A Novel Approach to Modernizing Large Aircraft Electrical Systems
2025 7th Global Power, Energy and Communication Conference (IEEE GPECOM2025), Bochum/ALMANYA, 11 Haziran 2025
HAKYEMEZ İBRAHİM,KELEŞ OĞUZ KAĞAN,BAĞRIYANIK MUSTAFA,KALENDERLİ ÖZCAN
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Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft
AIAA Aviation Forum and Exposition, Washington, Washington (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 2 Ağustos 2021
IMRAK RUMED, KARASELVİ EMRE, TUTKUN BÜLENT, NİKBAY MELİKE
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Loss-of-Control Prevention of an Agile Aircraft: Dynamic Command Saturation Approach
Journal of Guidance, Control, and Dynamics, Vol. 48, Şubat 2025, s. 13, ISSN: 0731-5090
ALTUNKAYA ÇAĞRI EGE,ÇATAK AKIN,KOYUNCU EMRE,ÖZKOL İBRAHİM
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A Comparative Study on Multi-Fidelity Sonic Boom Prediction for a Supersonic Aircraft
AeroBest 2021, An Eccomas Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, Lisbon (Virtual)/PORTEKİZ, 21 Temmuz 2021
YUSUF DEMİROĞLU, NİKBAY MELİKE
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The Vital Link: Using LabVIEW to Develop the Ground Processing Interface System (GPIS) Software for the C-5 Galaxy Aircraft
National Instruments (NI) Week 1998 [Poster Presentation & Proceedings recorded in a CD], Austin/AMERİKA BİRLEŞİK DEVLETLERİ, Vol. 1998, No. 246, 24 Ağustos 1998, s. 1-9
ÇİÇEK İSMAİL
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Thermomechanical Fatigue Analysis of an Aircraft Engine Turbine Blade
International Conference on Aircraft and Aerospace Structural Design (ICAASD-25), Roma/İTALYA, 9 Haziran 2025
TÜRKMEN HALİT SÜLEYMAN,KAYMAKSIZ MEHMET EMİN
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Multiple fault-based FDI and reconfiguration for aircraft engine sensors
Aircraft Engineering and Aerospace Technology, Vol. 89, No. 3, Mayıs 2017, s. 397-405, ISSN: 0002-2667
YAZAR IŞIL,ÇALIŞKAN FİKRET,KIYAK EMRE
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Turbulent Boundary Layer Noise of Fighter Aircraft Canopy
ICCFD12, 15 Temmuz 2024
ZAFER BAHA,KUŞ ALPEREN
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Digital-Twin Aircraft Performance and WindModeling Using Machine Learning
Boeing Technical Excellence Conference, 4 Temmuz 2019
UZUN MEVLÜT,KOYUNCU EMRE,İNALHAN GÖKHAN
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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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Investigation of Fluid Dynamics in Various Aircraft Wing Tank Designs Using 1D and CFD Simulations
Aerospace, Vol. 11, Haziran 2024, ISSN: 2226-4310
KARAHAN KEREM,ÇADIRCI SERTAÇ
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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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