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Vibrational genetic algorithm as a new concept in airfoil design
Aircraft Engineering and Aerospace Technology, Vol. 74, No. 3, Haziran 2002, s. 228-236, ISSN: 0002-2667
HACIOĞLU ABDURRAHMAN,OZKOL İBRAHİM
İbrahim Özkol Özgün Makale
Bending of Composite Cylindrical Shells with Circular Cutouts: Buckling and Failure Analysis
JOURNAL OF AIRCRAFT, Vol. 56, No. 4, Temmuz 2019, s. 1551-1564, ISSN: 0021-8669
ÇELEBİ MANSUR,GÜRDAL ZAFER,BLOM-SCHİEBER AGNES,WANTHAL STEVEN,RASSAİAN MOSTAFA,TATTİNG BRİAN,TÜRKMEN HALİT SÜLEYMAN
Halit Süleyman Türkmen Özgün Makale
Dynamic Multimode Response of Composite Plates to Sonic Boom and Blast Loadings
Journal of Aircraft, Vol. 45, No. 2, Mart 2008, s. 498-507, ISSN: 0021-8669
DOĞAN VEDAT ZİYA
Vedat Ziya Doğan Özgün Makale
Optimization of the PD coefficient in a flight simulator control via genetic algorithms
Aircraft Engineering and Aerospace Technology, Vol. 74, No. 2, Nisan 2002, s. 147-153, ISSN: 0002-2667
YURT SAİT,OZKOL İBRAHİM,KAYA METİN ORHAN,HACIZADE CENGİZ
İbrahim Özkol Özgün Makale
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
Vedat Ziya Doğan Özgün Makale
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
Levent Ali Kavurmacıoğlu Tam metin bildiri
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
İbrahim Özkol Özgün Makale
Localization and tracking of RF emitting targets with multiple unmanned aerial vehicles in large scale environments with uncertain transmitter power
2017 International Conference on Unmanned Aircraft Systems (ICUAS), Miami, FL/AMERİKA BİRLEŞİK DEVLETLERİ, 27 Temmuz 2017
HASANZADE MEHMET,HEREKOĞLU ÖMER,ÜRE NAZIM KEMAL,KOYUNCU EMRE,YENİÇERİ RAMAZAN,İNALHAN GÖKHAN
Emre Koyuncu Tam metin bildiri
Design of a Quad-Jet VTOL UAS for Heavy-lift Applications
2020 International Conference on Unmanned Aircraft Systems (ICUAS'20), 1 Eylül 2020, s. 875-882
TÜRKMEN ABDULLAH, ALTUĞ ERDİNÇ
Erdinç Altuğ Tam metin bildiri
Manufacturing and flight tests of a quadrotor UAS with tiltable rotors
2016 International Conference on Unmanned Aircraft Systems (ICUAS), Arlington, VA, USA/AMERİKA BİRLEŞİK DEVLETLERİ, 7 Haziran 2016
ŞENKUL FATİH,ALTUĞ ERDİNÇ
Erdinç Altuğ Tam metin bildiri robotik
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
Mehmet Şahin Özgün Makale
Formal intent based Flight Management System design for unmanned aerial vehicles
2014 International Conference on Unmanned Aircraft Systems (ICUAS), Orlando, FL/AMERİKA BİRLEŞİK DEVLETLERİ, 27 Mayıs 2014
TARHAN FARABİ AHMED,KOYUNCU EMRE,HASANZADE MEHMET,ÖZDEMİR UĞUR,İNALHAN GÖKHAN
Emre Koyuncu Tam metin bildiri
Estimated Time of Arrival Sensitivity to Aircraft Intent Uncertainty
5th IFAC Symposium on Control in Transportation Systems CTS 2018, Genoa/İTALYA, Vol. 51, No. 9, 6 Haziran 2018, s. 162-167
CASADO ENRİQUE, CİVİTA MARCO LA, UZUN MEVLÜT, KOYUNCU EMRE, İNALHAN GÖKHAN
Emre Koyuncu Tam metin bildiri
Active Vibration Control of Aircraft Wings Modeled as Thin-Walled Composite Beams Using Piezoelectric Actuation
ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers Digital Collection, MONTREAL/KANADA, 14 Kasım 2014
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Kaan Yıldız Tam metin bildiri
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
Kaan Yıldız Tam metin bildiri
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
Kaan Yıldız Tam metin bildiri
Thermal Stress Concentration in Plates from Different Materials
Journal of Aircraft, Vol. 49, No. 3, Mayıs 2012, s. 941-946, ISSN: 0021-8669
ABDULALİYEV Z, BAKİOGLU M, ATAOGLU S, KURTKAYA Z, GULLUOGLU AN
Şenol Ataoğlu Özgün Makale
A Novel Approach for Internet of Things Based Intelligent Weather Data Acquisition in Aircraft
Fifth International Symposium on Engineering, Artificial Intelligence and Applications (ISEAIA 2017), 1 Kasım 2017
SIRT DOĞU,SIRT MERVE,DAĞLARLI EVREN,ARIBAŞ ERKE
Doğu Sırt Tam metin bildiri
Energy Efficiency at Airports Through the Management of Aircraft De-Icing Fluid (ADF) by a High-Rate Anaerobic Treatment Process
Industrial Water 2018, 27 Kasım 2018, s. 62-63
ENGİZ GİZEM,SU ESRA,GÖMEÇ ÇİĞDEM
Çiğdem Gömeç Özet Bildiri
Comparative Evaluation of Biogas Recovery During Anaerobic Treatment of Aircraft Deicing Fluids at Increased Ratios in Domestic Wastewater
4th International Conference on Recycling and Reuse 2018 (RR2018), 24 Ekim 2018
GÖKTAŞ MURAT,ENGİZ GİZEM,SU ESRA,GÖMEÇ ÇİĞDEM
Çiğdem Gömeç Özet Bildiri

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