American Journal of Mechanical and Industrial Engineering

Volume 1, Issue 1, July 2016

  • Material Selection for High Pressure (HP) Turbine Blade of Conventional Turbojet Engines

    Ikpe Aniekan Essienubong, Owunna Ikechukwu, Patrick. O. Ebunilo, Ememobong Ikpe

    Issue: Volume 1, Issue 1, July 2016
    Pages: 1-9
    Received: 5 June 2016
    Accepted: 13 June 2016
    Published: 23 June 2016
    DOI: 10.11648/j.ajmie.20160101.11
    Abstract: Turbojet engine can be divided into three major sections including the compressor, combustion chamber and the gas turbine section. The relatively high temperature gas that passes through the high pressure turbine stages of a turbojet engine from the combustion chamber has a direct effect on the performance and efficiency of the gas turbine, which m... Show More