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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
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
Reliability based aeroelastic optimization of a composite aircraft wing via fluid structure interaction of high fidelity solvers
IOP Conference Series: Materials Science and Engineering, Vol. 10, No. 1, Temmuz 2010, s. 12037, ISSN: 1757-899X
NİKBAY MELİKE,NECATİ FAKKUSOGLU,MUHAMMED NASİF KURU
Melike Nikbay Özgün Makale
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
Solid rocket motor design using a surrogate model
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 90, No. 7, Ekim 2018, s. 1104-1127, ISSN: 1748-8842
TOLA CEYHUN,NİKBAY MELİKE
Melike Nikbay 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
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
İbrahim Özkol Özgün Makale
Assessment of NOx emissions of the Scimitar engine at Mach 5 based on a thermodynamic cycle analysis
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, Vol. 45, No. 5, Ocak 2020, s. 3632-3640, ISSN: 0360-3199
TANBAY TAYFUN,UCA MUHAMMED BİŞAR,DURMAYAZ AHMET
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
Ahmet Cansız Tam metin bildiri
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
Erke Arıbaş Tam metin bildiri
Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover Part II
, Aircraft Engineering and Aerospace Technology: An International Journal, 2007
ÖZGE ÖZDEMİR ÖZGÜMÜŞ,KAYA METİN ORHAN
Metin Orhan Kaya Özgün Makale
Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: part II. Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover
Aircraft Engineering and Aerospace Technology, Vol. 79, No. 3, Mayıs 2007, s. 231-237, ISSN: 0002-2667
ÖZDEMİR ÖZGÜMÜŞ ÖZGE, KAYA METİN ORHAN
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
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
A review of in flight detection and identification of aircraft icing and reconfigurable control
PROGRESS IN AEROSPACE SCIENCES, Vol. 60, Temmuz 2013, s. 12-34, ISSN: 0376-0421
ÇALIŞKAN FİKRET,HACIZADE CENGİZ
Fikret Çalışkan Özgün Makale
How does inventory performance affect operational performance? An example from US space vehicles and aircraft parts industries
2017 8th International Conference on Recent Advances in Space Technologies (RAST), İSTANBUL/TÜRKİYE, 19 Haziran 2017, s. 291-294
HANÇERLİOĞULLARI GÜLŞAH,KÖKSALMIŞ EMRAH,ÇALIŞIR FETHİ
Fethi Çalışır Tam metin bildiri
Micro scale synthetic jet actuator flow simulation with characteristic based split method
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 3, Ocak 2009, s. 239-246, ISSN: 0002-2667
CELİK BAYRAM, EDİS FİRAT OGUZ
Fırat Oğuz Edis Özgün Makale
Multidisciplinary Code Coupling for Analysis and Optimization of Aeroelastic Systems
AIAA Journal of Aircraft, Vol. 46, No. 6, 2009, s. 1938-1944
NİKBAY MELİKE,LEVENT ONCU,AHMET AYSAN
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
Atomistic simulation of micro scale adiabatic piston problem
Aircraft Engineering and Aerospace Technology, Vol. 81, No. 6, Ocak 2009, s. 499-507, ISSN: 0002-2667
SENGİL NEVSAN, EDİS FİRAT OGUZ
Fırat Oğuz Edis Özgün Makale

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