Which is our task

In a wide range of aerospace, automotive and indastrial structure our task is to support any structutal design topic, from the concept until final assembly configuration.

Linear Static Analysis
In the most cases is considered the quicker approach to FE simulation. Provide an immediate and general idea �of component or assembly behavior.

Non Linear Static Analysis
Often allow solutions for slightly more complicated problems where contact analysis is required. Linear contact, or surface contact problems offer a more realist behavior for assembled parts.

Modal Analysis
Most of cases is used as preliminary check of structures to evaluate eingvalues, vibrations modes and frequencies.

Non Linear Material Analysis
When high loads are applied on the structures, where failure are expected, this analysis gives the possibility to perform material behavior in the plastic regions, even far �from yielding point.

Allows to check static behavior of parts loaded by an unexpected load which causes an instability on the component.

Where the structure is affected by external vibrations, due for example to Engine Vibration Frequency, stresses on parts can be evaluated.

All parts are often loaded by fatigue spectrum which can cause unexpected failure where crack can occur. Classical methods or up to date software can predict life component, depending on treatments, surface status etc.

STRUCTURES

Structural Analysis

FEM approach provides a full range of analysis as:

• Linear static analysis
• Nonlinear static analysis
• Modal analysis
• Non Linear material analysis
• Linear dynamic analysis
• Fatigue analysis

AEROVEN ug multidisciplinary experience guarantees reliable and consistent simulations, short time in developing models using the proper tool for the specific problem.

Parallel to the most advanced FEM techniques AEROVEN ug is able to perform preliminary structural checks and preliminary designs by means of suitable instruments of calculation developed from preliminary concept, to full design until final test.

FE MODEL

DESCRIPTION

• Before Analysis

Every analysis performed starts from an attentive check of Geometry part and surrounding structure, in order to simulate the structural problem as closer as to reality. Detailed FE models are prepared, checked and finalized according to all requirements.

• Deformation from Analysis

Results, maximum allowable deformations and displacements are computed. .

• Stress Results from Analysis

Results, stress and strain are computed, on critical locations. Elastic and Plastic material are used depending on specific topic.

• Test and validation

When possible FE models, for dedicated configurations, are compared and validated by Test Results.