The Digital Twin Blog.
This Tips & Trick shows how you can overlay the critical ply ID and load case ID on laminate element contour plots using Advanced Post Report in NX Laminate Composites (NXLC).
This tips and Tricks shows how to use the Mechanical Load Summary command in NX to compute the total forces and moments for the active structural analysis solutions or sub cases.
This tips and tricks shows how to use NX Laminate Composites to identify a core ply and to automatically compute 13 and 23 core shear failure index, margin of safety, and strength ratio results.
Often, one conducts a CFD analysis of a system, taking into account fans, obstructions, multiple components and the surrounding environment.
This Tips & Trick shows how to use the Combined Load-cases functionality in NX, which allows you to create combinations of linear load case results, thereby avoiding the need to pre-define and solve all the required combinations.
This Tips & Trick shows how you can define your own ply and interlaminar failure theories in NX Laminate Composites.
This Tips & Trick shows how to use an NX formula field and face’s isolines to easily define a spatially-varying pressure load.
This Tip & Trick will explain the difference between the failure index and strength ratio and their respective applicability when using composite material quadratic failure criteria.
This Tip & Trick shows how to use the results from a thermal simulation to create a temperature load in a structural simulation using fields.
An Isotropic blockage is prescribed to the heat exchanger air volume using the Head Loss and Permeability method.
This post-processing Tip & Trick will show how to calculate the stress margins of safety of a structure under a static pressure load, and then how to plot the margins and locate the critical areas of the part.
Global expert in numerical simulations for the world of engineering, Maya HTT becomes a member of the Consortium Innovee.
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