AEROSPACE STRUCTURE ANALYSIS

GURUCAD AEROSPACE DIVISION

BREAKING THE KNOWLEDGE LIMITS IN AEROSPACE INDUSTRY


GURUCAD has a very strong know-how in the area of Stress Analysis using modern calculation methods and tools among them, there are also GURUCAD developed tools for geometry simplification in CATIA V5, exchange of FEM data from CATIA V5 to PATRAN and reverse, template macro based Word Stress Reports... All this assure our customers that their structure will be weight-optimised and the stress analysis costs will be kept under control.

GURUCAD provides the following Analysis & Simulation Services:
  • FE modeling & meshing (0D, 1D, 2D and 3D Elements)
  • Finite Element Idealization (fittings, inserts, fasteners, wing/fuselage primary structure and specialized structural models)
  • Creation and interpretation of Finite Element Models
  • Structural analysis of both composite and metallic structures
  • Finite element calculation of different loading cases
  • Modeling of composite materials
  • Fatigue analysis
  • Damage tolerance analysis
  • Crack propagation (fracture) analysis
  • Thermal analysis
  • Impact studies
  • Design and analysis loops with optimization purpose
  • Expand/review/refine existing finite element models (FEM)
  • New finite models from geometric models (CAD – geometry simplification)
  • Hand calculation (rivets, buckling and stress justification)
  • Interpretation of the results
  • Presentation of the result to the customer
  • Development of methods and tools in the area of Stress Analysis
  • Creation of Justification Stress Reports
  • Creation of Substantiation Stress Reports
  • Creation of Interface Loads Reports
  • Review of concessions

For Stress Worpackages we conduct in-house, we use the following software:

  • HyperWorks (HyperMesh, RADIOSS, HyperView, OptiStruct)
  • Nastran-Patran

In order to meet your requirements, we are also capable of using other software, as needed:

  • ANSYS
  • COSMOS

FLYERS:


GURUCAD AEROSPACE DIVISION


Aerospace Secondary Structure Optimisation COSMOS - SOLID WORKS

Aerospace Secondary Structure Analysis Optimisation CATIA V4

Aerospace Secondary Structure Analysis NASTRAN-PATRAN 2005 - Von Mises

Hydraulic Brackets Analysis NASTRAN-PATRAN 2005 - Displacements