EXAMPLES OF COMPLETED PROJECTS. AVIATION.

  • Helicopter composite fuselage stress analysis.
    A Private Helicopter Designer Project

      Software: CATIA V5R21, NASTRAN, PATRAN 2008R2, Excel 2007

      Load Cases were determined in accordance with FAR23.
      FE model was created and analysed.
      Global FE model was created. Colposite materials were set.
      Some critical parts were modeled using the technique of stiching local FE model into a global one.
      Hand stress analysis calculations were performed.

  • Light Sport Aircraft metal fuselage stress analysis.
    Company: "Aeroprakt"

      Software: CATIA V5R16, FEMAP 9.3

      FE model was created and analysed.
      Hand stress analysis calculations were performed for some parts.

  • Light Sport Aircraft Flap release lever designing.
    Company: "Aeroprakt"

      Software: Pro/ENGINEER, FEMAP 9.3

      CAD Solid model was created
      FE model was created and analysed.
      CNC programming was performed

  • Light Sport Aircraft Landing Gear Main Leg Stress Analysis.
    Company: "Aeroprakt"

      Software: Pro/ENGINEER, FEMAP 9.3

      FE model was created and analysed.

  • Ultralight Aircraft Tail Boom Buckling Analysis.
    Company: "Aeroprakt"

      Software: Pro/ENGINEER, FEMAP 9.3

      FE model was created.
      Buckling load obtained using FE analysis methods was compared with test data.

  • FE analysis of a light aircraft landing gear main leg.

    A Private Homebuilt Aircraft Designer Project.

      Software: CATIA V5R20, NASTRAN, PATRAN

      The possibility of mounting a new design landing gear main leg was tested. The conclusion was made about the main leg geometry.
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