Zobrazeno 1 - 10 of 151 pro vyhledávání: '"İbrahim OZKOL"'
1
Akademický článek
Thermal Structural Design Aspects of Military Aircraft
Autor: Mustafa Tolga Yavuz, Ibrahim Ozkol
Publikováno v: Havacılık ve Uzay Teknolojileri Dergisi, Vol 17, Iss 1, Pp 124-158 (2024)
This study presentsthe thermal-structural design aspects of military aircraft, exploring key components such as the evolution of fighters, high-temperature effects, airframe construction, and the role of thermal structural tests. From the early days
Externí odkaz: https://doaj.org/article/0cd1c16047764d2697dec8de083549c8
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2
Akademický článek
Operational Improvements to Reduce the Climate Impact of Aviation—A Comparative Study from EU Project ClimOP
Autor: Zarah Lea Zengerling, Sara Dal Gesso, Florian Linke, Maximilian Clococeanu, Volker Gollnick, Patrick Peter, Sigrun Matthes, Baris Baspinar, Ibrahim Ozkol, Mahdi Noorafza, Paul Roling, Elena Branchini, Mattia Grampella, Carlo Abate, Alessandra Tedeschi
Publikováno v: Applied Sciences, Vol 13, Iss 16, p 9083 (2023)
Aviation significantly contributes to anthropogenic radiative forcing with both CO2 and non-CO2 emissions. In contrast to technical advancements to mitigate the climate impact, operational measures can benefit from short implementation times and thus
Externí odkaz: https://doaj.org/article/5a350ae4f84d48749d6d8ed80dc30e8b
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3
Akademický článek
Stick-Free Flight Stability Problem Revisited: A Modeling and Simulation Approach
Autor: Ege Cagri Altunkaya, Ibrahim Ozkol
Publikováno v: Aerospace, Vol 10, Iss 3, p 234 (2023)
The stick-free flight stability is an old-fashioned and non-progressive issue; nevertheless, it is still existent and of significant importance to the design of aircraft whose control system is reversible. The existence of the problem necessitates a
Externí odkaz: https://doaj.org/article/2f1b831019c0401c822864e8b31d9808
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6
Regression Rate Enhancement of Hybrid Rockets by Introducing Novel Distributed Tube Injector
Autor: M. Arif Karabeyoglu, Mehmet Kahraman, Ibrahim Ozkol
Publikováno v: Journal of Propulsion and Power. 38:200-211
Low fuel regression rate is one of the major drawbacks of hybrid rocket motors. In this study, a novel injector concept is proposed to provide a substantial enhancement in the fuel regression rate....
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::b3b2a0af21f37f7f567e135ac78a12ab
https://doi.org/10.2514/1.b38417
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9
Akademický článek
Magnetohydrodynamic Flow of Liquid-Metal in Circular Pipes for Externally Heated and Non-Heated Cases
Autor: Atilla Altintas, Ibrahim Ozkol
Publikováno v: Journal of Applied Fluid Mechanics, Vol 8, Iss 3, Pp 507-514 (2015)
The Computational Fluid Dynamics (CFD) study of external magnetic field effect on the steady, laminar, incompressible flow of an electrically conducting liquid-metal fluid in a pipe has been performed. The MHD Module of ANSYS Fluent commercial progra
Externí odkaz: https://doaj.org/article/b318675595654031a2ffa784400bc63e
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10
Stick-free Flight Stability Problem Revisited: A Modeling and Simulation Approach
Autor: Ege Cagri Altunkaya, Ibrahim Ozkol
Publikováno v: Aerospace
Volume 10
Issue 3
Pages: 234
The stick-free flight stability is an old-fashioned and non-progressive issue; nevertheless, it is still existent and of significant importance to the design of aircraft whose control system is reversible. The existence of the problem necessitates a
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d598d576a06a0d7b1e5776aa5a5a4b97
https://doi.org/10.20944/preprints202212.0180.v1
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