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Özel Aralık Girişi

Intelligent Based Aircraft Engine Health Monitoring Improving Aircraft Engine Maintenance Effectiveness and Reliability
Saarbrücken/ALMANYA, 2011, LAP LAMBERT Academic Publishing GmbH&Co.KG
DEMİRCİ ŞEREF, HAJİYEV CHİNGİZ
Cengiz Hacızade Bilimsel Kitap
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
Fikret Çalışkan Özgün Makale
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
Metin Orhan Kaya Özgün Makale
Image Based and Hybrid Visual Servo Control of an Unmanned Aerial Vehicle Recent Developments in Unmanned Aircraft Systems
2012, Springer
ZEHRA CEREN,ALTUĞ ERDİNÇ
Erdinç Altuğ Bilimsel KitapKitap Bölümü
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
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
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
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
Fikret Çalışkan Özgün Makale
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
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
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
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
Oktay Çiçek Özgün Makale
Aircraft Scheduled Airframe Maintenance and Downtime Integrated Cost Model
ADVANCES IN OPERATIONS RESEARCH, Haziran 2016
SALTOĞLU REMZİ,HUMAİRA NAZMİA,İNALHAN GÖKHAN
Gökhan İnalhan Özgün Makale
Optimization of connection analysis in aircraft structures
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
EVREN FATMA NUR,OZKOL İBRAHİM
İbrahim Özkol Tam metin bildiri
Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
Algorithms, Temmuz 2022, ISSN: 1999-4893
YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, NİKBAY MELİKE
Şıhmehmet Yıldız Özgün Makale
Adaptive control of a tilt roll rotor quadrotor UAV
2014 International Conference on Unmanned Aircraft Systems (ICUAS), 27 Mayıs 2014
FATİH ŞENKUL,ALTUĞ ERDİNÇ
Erdinç Altuğ Tam metin bildiri
Aeroelastic Analysis of a Tapered Aircraft Wing
4th Ankara International Aerospace Conference, Ankara/TÜRKİYE, 10 Eylül 2007
EKEN SEHER, ÖZDEMİR ÖZGE, KAYA METİN ORHAN
Seher Eken Tam metin bildiri
Learning-based Aircraft Trajectory Planning Enhancement
AIAA Scitech 2019 Forum, San Diego/AMERİKA BİRLEŞİK DEVLETLERİ, 7 Ocak 2019
ALİZADEH ALİ,HUMAİRA NAZMİA,KOYUNCU EMRE
Emre Koyuncu Tam metin bildiri
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
Seher Eken Tam metin bildiri
Modeling and Control of a Novel Tilt Roll Rotor Quadrotor UAV
International Conference on Unmanned Aircraft Systems (ICUAS'13)
FATİH ŞENKUL, ERDİNÇ ALTUĞ
Erdinç Altuğ Tam metin bildiri

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