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
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Error analysis and motion determination of a flight simulator
Aircraft Engineering and Aerospace Technology, Vol. 76, No. 2, Nisan 2004, s. 185-192, ISSN: 0002-2667
YURT SAİT,OZKOL İBRAHİM,HACIZADE CENGİZ
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Experimental and Numerical Investigation of a Swirl Stabilized Premixed Methane Air Flame
Aircraft Engineering and Aerospace Technology, Bingley/İNGİLTERE, Vol. 86, No. 3, Nisan 2014, s. 215-224, ISSN: 0002-2667
KAYNAROĞLU B, TUNÇER O
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Mode decoupling robust eigenstructure assignment applied to the lateral-directional dynamics of the F-16 aircraft
AEROSPACE SCIENCE AND TECHNOLOGY, Vol. 77, Haziran 2018, s. 677-687, ISSN: 1270-9638
ALBOSTAN ONUR,GÖKAŞAN METİN
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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
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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
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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
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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
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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
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The effects of the use of single task-oriented maintenance concept and more accurate letter check alternatives on the reduction of scheduled maintenance downtime of aircraft
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
SENTURK CANER,OZKOL İBRAHİM
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Sugeno and Mamdani based Fuzzy Inference Approaches for Aircraft Pitch Control
International Conference on Mathematics and Mathematics Education (ICMME), URFA/TÜRKİYE, 11 Mayıs 2017
ÖZTÜRK MUHAMMET,BAYEZİT İSMAİL,OKUDAN MEHMET EMİN,OZKOL İBRAHİM
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Evaluation of critical parameters in the design of a trainer aircraft landing gear
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE), 22 Temmuz 2017
ÇETİNKAYA BURHAN,OZKOL İBRAHİM
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Implementation of Propulsion System Integration Losses to a Supersonic Military Aircraft Conceptual Design
AIAA Propulsion and Energy 2021 Forum, Virtual/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ağustos 2021
KARASELVİ EMRE, NİKBAY MELİKE
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Multifidelity Sonic Boom Minimization of A Supersonic Aircraft by Parametric Wing Shape Design
AIAA Scitech Forum, Tennessee (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 11 Ocak 2021
YUSUF DEMİROĞLU, YILDIZ ŞIHMEHMET, NİKBAY MELİKE
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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
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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
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Intercomparison and assimilation of NO2 retrievals obtained from satellite SCIAMACHY aircraft and ground observations into a regional scale air quality model CMAQ DDM for the continental U S
7th International Conference on Air Quality - Science and Application, İstanbul/TÜRKİYE, 24 Mart 2009
KAYNAK BURÇAK,HU YONGTAO,MARTİN RANDALL V,RUSSELL ARMİSTEAD G
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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
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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
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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
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