Study of Refractory Materials Usage in Aerospace Engines Technology

Manna, Ali Hafiz Omer; Mohammed, Mazin Ahmed Ali; Ahmed, Mohamed Elsir Elkhider; Ali, Mussab Omer Elsir; Supervisor-, Abdalrahem Saad Omer

dc.contributor.author	Manna, Ali Hafiz Omer
dc.contributor.author	Mohammed, Mazin Ahmed Ali
dc.contributor.author	Ahmed, Mohamed Elsir Elkhider
dc.contributor.author	Ali, Mussab Omer Elsir
dc.contributor.author	Supervisor-, Abdalrahem Saad Omer
dc.date.accessioned	2018-01-21T13:19:50Z
dc.date.available	2018-01-21T13:19:50Z
dc.date.issued	2017-10-01
dc.identifier.citation	Manna, Ali Hafiz Omer.Study of Refractory Materials Usage in Aerospace Engines Technology/Ali Hafiz Omer Manna...{etal};Abdalrahem Saad Omer.-Khartoum : Sudan University of Science and Technology, College of Engineering,2017.-56 p. :ill;28cm.- Bachelors search.	en_US
dc.identifier.uri	http://repository.sustech.edu/handle/123456789/20109
dc.description	Bachelors search	en_US
dc.description.abstract	When engine parts are subjected to a high temperature, their life time and performance will reduce due to the defects result from that high temperature. This report shows the definition of refractory materials, its properties and the effect of using them in rockets engines (nozzles) and aircrafts engines (turbine blades). A turbine blade studied by using ANSYS 16.0 software in order to show the effect of thermal barrier coating which expose noticeable reduction in the temperature penetrating the blade’s layers, hence the thermal barrier coating increase the durability of the blade by decreasing the temperature subjected to the basic blade material. Supersonic turbine blade materials percentage displayed by using X-Ray florescent test.	en_US
dc.description.sponsorship	Sudan University of Science and Technology	en_US
dc.language.iso	en	en_US
dc.publisher	Sudan University of Science and Technology	en_US
dc.subject	Materials Usage in Aerospace	en_US
dc.subject	Study of Refractory	en_US
dc.subject	Engines Technology	en_US
dc.title	Study of Refractory Materials Usage in Aerospace Engines Technology	en_US
dc.type	Thesis	en_US