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Tag Archives: FEM

Strength Criteria of Composite Material supported by FEM analysis

Posted on February 17, 2019 by Aerospace Engineering

Strength Criteria of Composite Material supported by FEM analysis Continue reading →

Posted in FEM - Analysis | Tagged analysis, BDF, Composite, Criteria, failure, FEM, hill, Hoffman, index, Lamina, material, Max, MSC, NASTRAN, patran, PCOMP, SOL101, strain, strength, Stress, Tsai, Tsai-Hill, Tsai-Wu, Wu | Leave a comment

Static Condensation – FEM Analysis

Posted on January 7, 2019 by Aerospace Engineering

Background Theory With “condensation” is indicated a procedure adopted for the structural analysis to carry out a matrix of stiffness … Continue reading →

Posted in FEM - Analysis | Tagged analysis, Condensation, DFEM, DMIG, EXTSEOUT, FEM, GFEM, Guyan, KAAX, Matrix, mes sewing, mesh, NASTRAN, PAX, Procedure, RBE3, reduction, SEW, sewing, SOL101 | Leave a comment

Non linear Buckling with FEM approach

Posted on September 20, 2016 by Aerospace Engineering

Buckling analysis assesses the stability characteristics of a structure. An accurate solution to a buckling problem requires more efforts than … Continue reading →

Posted in FEM - Analysis | Tagged 105, 106, Abaqus, buckling, FEM, linear, NASTRAN, Non, SOL | Leave a comment

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