Data-driven aircraft performance models for improving baseline fuel estimations
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2018
MUHAMMED EMRE SARIGÖL
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Energy-based metrics for fighter aircraft assessment
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2018
NAZMIA HUMAIRA
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Modeling, simulation, and test flight validation of a fixed-wing unmanned aircraft system
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2019
ERTUĞRUL BARIŞ ÖNDEŞ
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Modelling, control and implementation of an unmanned vertical take-off and landing aircraft
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2014
FARABİ AHMED TARHAN
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Simulator training and practice for reducing the effect of pilots in aircraft accidents
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2019
ULAŞ BERK BAYRAMOĞLU
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Geopolitics of aviation, decision of a potential aircraft and economical modelling of a helicopter maintenance center in related region
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2019
BARAN EMRE SONUÇ
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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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Heuristic Algorithms for Aircraft Sequencing Problem
33rd International Annual Conference of the American Society for Engineering Management, VIRGINIA BEACH/AMERİKA BİRLEŞİK DEVLETLERİ, 17 Ekim 2012, s. 773-779
HANÇERLİOĞULLARI KÖKSALMIŞ GÜLŞAH, GHAITH RABADI, AMEER AL SALEM, KAHRBECHE MOHAMED
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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
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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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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
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Reliability Based Multidisciplinary Optimization of Aeroelastic Systemswith Structural and Aerodynamic Uncertainties
AIAA Journal of Aircraft, Vol. 50, No. 3, 2013, s. 798-715, ISSN: 0021-8669
NİKBAY MELİKE,MUHAMMET NASİF KURU
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Integrating Analytical Aeroelastic Instability Analysis into Design Optimiza tion of Aircraft Wing Structures
TWMS Journal of Applied and Engineering Mathematics, Vol. 1, No. 2, 2011, s. 237-253
NİKBAY MELİKE,PİNAR ACAR
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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
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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
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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
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Reliability Based Design Optimisation of an Aircraft Wing Structure with High Fidelity Modelling
International Journal of Design Engineering, Vol. 3, No. 3, 2011, s. 247-259
NİKBAY MELİKE,MUHAMMET NASİF KURU,SEMRA BAYAT,NECATİ FAKKUSOGLU
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