Project epsilon

Client: Aerospace Domestic Supplier – Analysis

Need: CAE analysis of gas turbine for various flight load conditions

Outcome:

  • 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