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Özel Aralık Girişi

Decentralized learning-based planning for multiagent missions in the presence of actuator failures
2013 International Conference on Unmanned Aircraft Systems (ICUAS), 28 Mayıs 2013
ÜRE NAZIM KEMAL,CHOWDHARY GİRİSH,CHEN YU FAN,CUTLER MARK,HOW JONATHAN P,VİAN JOHN
Nazım Kemal Üre 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
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
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
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
Optimal Control Procedure Application for Dynamic Response of Adaptive Aircraft Wings Modeled as Thin-Walled Composite Beams
Applied Mechanics and Materials, Vol. 798, Ekim 2015, s. 292-296, ISSN: 1662-7482
YILDIZ KAAN, EKEN SEHER, KAYA METİN ORHAN
Kaan Yıldız Özgün Makale
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
Erdinç Altuğ 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
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
Alim Rüstem Aslan Teknik Not
Design and Development of a New Integrated Communication System for C-5 Galaxy Aircraft
Transactions of the SDPS. Journal of Integrated Design & Process Science, Vol. 2, No. 4, Mart 1999, s. 41-51, ISSN: 1092-0617
ÇİÇEK İSMAİL, SCHAFER DAVİD
Aerodynamic characteristics of external store configurations at low speeds
Journal of Aircraft, Vol. 32, No. 1, Ocak 1995, s. 161-170, ISSN: 0021-8669
ÖZCAN OKTAY,ÜNAL MEHMET FEVZİ,ASLAN ALİM RÜSTEM,BOZKURT YÜKSEL,NH AYDIN
Alim Rüstem Aslan Özgün Makale
Automated troubleshooting tools for minimizing downtime and reducing the labor and materialcosts of C-5 aircraft
AUTOTESTCON 2004, PROCEEDINGS, 20 Eylül 2004, s. 504-510, ISSN: 1088-7725
VİLLAREAL CARLOS,ÇİÇEK İSMAİL
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
Sertaç Çadırcı Tam metin bildiri
Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft
AIAA Aviation 2021 FORUM, 2 Ağustos 2021
IMRAK RUMED, KARASELVİ EMRE, TUTKUN BÜLENT, NİKBAY MELİKE
Vibration Considerations for the Installation of Portable Equipment on Military Aircraft
Society for Design and Process Science (SDPS) Integrated Design & Process Technology (IDPT) Symposium on System Design and Software Engineering, İzmir/TÜRKİYE, Vol. 1, No. 5, 28 Haziran 2004, s. 142-151, ISSN: 100-89
ÇİÇEK İSMAİL, ERTAS ATİLA
İsmail Çiçek Tam metin bildiri Titreşim
Application of Weibull Distribution Method for Aircraft Component Life Estimation in Civil Aviation Sector
Journal of Traffic and Logistic Engineering, Temmuz 2017
FİDANOĞLU MELİH,GUNGOR UFUK,OZKOL İBRAHİM,KÖMÜRGÖZ KIRIŞ GÜVEN
Electrical System Design for Very Light Aircraft
ISUDEF 2021 (International Symposium on Unmanned Systems and the Defense Industry) Program, Washington/AMERİKA BİRLEŞİK DEVLETLERİ, 25 Ekim 2021
ALUÇ MERVE, KÖMÜRGÖZ KIRIŞ GÜVEN
Güven Kömürgöz Kırış Tam metin bildiri
Micro‐scale synthetic‐jet actuator flow simulation with characteristic‐based‐split method
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 3, Mayıs 2009, s. 239-246, ISSN: 0002-2667
ÇELİK BAYRAM,EDİS FIRAT OĞUZ
Bayram Çelik Özgün Makale
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
Burçak Kaynak Tezel Özgün Makale

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