What is the best method for determining fiber load in a composite material?

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SUMMARY

The best method for determining fiber load in composite materials with aligned fibers at alternating angles involves using Classical Laminate Theory (CLT). This analytical approach is foundational in composite analysis and is typically covered in introductory courses. Industry professionals, particularly in aerospace, utilize tools like NX Nastran for structural analysis, which incorporates these techniques when defining plies for plate elements. Accurate strain computation in the fiber direction is critical for effective load determination.

PREREQUISITES
  • Classical Laminate Theory (CLT)
  • Composite material mechanics
  • NX Nastran for structural analysis
  • Understanding of strain measurement techniques
NEXT STEPS
  • Research Classical Laminate Theory applications in composite materials
  • Explore NX Nastran documentation for ply definition techniques
  • Study analytical solutions for fiber load determination in composites
  • Investigate industry standards for composite material testing and analysis
USEFUL FOR

Aerospace engineers, composite material researchers, and professionals involved in structural analysis of composite materials will benefit from this discussion.

muzialis
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Hello there,

I am wondering if some specilalist would point in me in the direction of procedures to determine the load in a fiber in a composite material made of aligned fibers (let's say at alternating angles $$+/- \alpha$$).
I understand you could simply compute the strain in a convenient direction for a "homogenized" composite material, rotate in the fiber direction to obtain the strain in the fiber direction, but I am not so sure about the accuracy of this procedure.
I am looking for analytical solutions, and I am interested in Industry standards too. I am surprised how difficult it is tio find something.

Many thanks and have a good day
 
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Experimental Characterization of Advanced Composite Materials, Third Edition by Leif Carlsson, Donald F. Adams and R. Byron Pipes (Oct 29, 2002)
 
The approach you mentioned is part of Classical Laminate Theory (or Classical Laminate Analysis). It's usually covered in a basic intro to composites course, so I think it's the standard starting point for composite analysis.

I work in aerospace doing composite stress analysis and we use NX Nastran for our structural analysis. I'm pretty sure that when you define plies for plate elements, it uses this technique or a variation on it.
 

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