Project epsilon

Aerospace Domestic Supplier – Analysis


CAE analysis of gas turbine for various flight load conditions


  • Analysis of the Gas turbine engine for various flight loads was carried out for a Domestic customer, the details of which are as indicated below:
    • Solid Meshing activities done using only hexahedral elements
    • Integration of individual FE modeled parts to obtain the complete engine assembly
    • Analysis activities for the entire assembly consisting of static linear and non-linear, thermal, dynamic, as well as optimization
    • Generation of detailed stress report

Tool used:

MSC Nastran & Hyper Mesh

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