Investigation of Blending of RAP and RAS binder into virgin binder at Mixture level using fatigue tests and image correlation

Date

2016-01-14

Author

Kutay, Muhammed Emin
Mogawer, Walaa
Öztürk, Hande Işık
Austerman, Alexander
Krcmarik, Michael

Metadata

Show full item record

Item Usage Stats

24
views

0
downloads

URI

https://hdl.handle.net/11511/84816

Collections

Unverified, Conference / Seminar

Suggestions

OpenMETU
Core

Investigation of fatigue behavior of a high strength lower bainitic structure in 60SIMN5 steel via a modified testing method Uluğ, Emirhan; Ögel, Bilgehan; Department of Metallurgical and Materials Engineering (2019) A steel with high silicon content can yield carbide-free bainite after an isothermal bainitic transformation. In this thesis study, fatigue behavior of a high strength carbide-free lower bainitic structure, which was produced from 60SiMn5 steel, was investigated. The fatigue tests of the same steel with tempered martensitic microstructure were also carried out for comparison purposes. Before fatigue testing, the mechanical properties of the specimens were also determined, which include hardness, yield stren...
Investigation of flowfield characteristics due to shock wave-boundary layer interaction on compression decompression corners using les Karpuzcu, Irmak Taylan; Sert, Cüneyt; Department of Mechanical Engineering (2019) Shock wave boundary layer interactions occur in industrial flows where the flow is transonic, supersonic or hypersonic and there is an incoming boundary layer present. Many of the air crafts such as planes, rockets, missiles, re-entry vehicles, and supersonic wind tunnels experience shock wave boundary layer interactions. These interactions can take place on an air craft at several different places such as the air intakes, ramps, forebody and fins, and also the diffuser section of a supersonic wind tunnel. ...
Investigation of effects of bird strike on wing leading edge by using explicit finite element method Dede, Oğuzhan; Kayran, Altan (null; 2015-09-10) In aviation industry, bird strike problem causes structural damage and threats to flight safety. Nowadays, designed and produced aircraft have to satisfy “safe flight and landing” requirements. The behavior of the aircraft components during bird strike have to be investigated by numerical methods or experiments. Results obtained from numerical analysis and /or experiments have to be carefully studied to optimize the aircraft structures. The main aim of this study is to apply the explicit finite element anal...
Investigation of Relationship between Aggregate Shape Parameters and Concrete Strength Using Imaging Technigues Özen, Murat; Yaman, İsmail Özgür; Güler, Murat (2008-09-15)
Investigation of effects of bird strike problem on wing leading edge by using explicit finite element method Dede, Oğuzhan; Kayran, Altan; Department of Aerospace Engineering (2015) In aviation industry, bird strike problem causes structural damage and threats to flight safety. Nowadays, designed and produced aircraft have to satisfy “safe flight and landing” requirements. The behavior of the aircraft components during bird strike have be to investigated by numerical methods or experiments. Results obtained from numerical analysis and /or experiments have to be carefully studied to optimize the aircraft structures. However, experiments of bird strike are very costly and require qualifi...

Citation Formats

M. E. Kutay, W. Mogawer, H. I. Öztürk, A. Austerman, and M. Krcmarik, “Investigation of Blending of RAP and RAS binder into virgin binder at Mixture level using fatigue tests and image correlation,” 2016, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/84816.