Compression or Tensile on Fiberglass

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SUMMARY

The discussion centers on the structural analysis of fiberglass under compressive loading from an aluminum frame. The tensile strengths of the fiberglass are specified as 380 MPa for the warp direction and 300 MPa for the weft direction, with a fiber volume of 50%. The user seeks to understand if the compressive load will exceed these specifications and whether Roark's 'Stress and Strain' can be applied to composite materials. The user is particularly interested in using Case No. 8 from Roark's for their calculations.

PREREQUISITES
  • Understanding of fiberglass material properties, specifically tensile strength.
  • Familiarity with Roark's 'Stress and Strain' for structural analysis.
  • Basic knowledge of composite material behavior under load.
  • Experience with finite element analysis (FEA) software for complex stress calculations.
NEXT STEPS
  • Research the application of Roark's formulas to composite materials.
  • Learn about finite element analysis (FEA) tools suitable for composite structures.
  • Study the effects of bending stresses on fiberglass panels.
  • Explore advanced composite material mechanics and their failure modes.
USEFUL FOR

Structural engineers, materials scientists, and students in engineering disciplines focusing on composite materials and their applications in load-bearing structures.

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Homework Statement



A piece of aluminum as shown in the picture is applying a compressive force on the fiberglass material. I need to know if the loading material will exceed the specification of the fiberglass material.

sample.jpg



Homework Equations



Properties of fiberglass
Tensile strength Monolayer (Warp): 380 MPa
Tensile strength Monolayer (Weft): 300 MPa

Fiber Volume: 50%

Properties of resin
Tensile strength: 30 MPa

Volume: 50%


The Attempt at a Solution



My question is, since the loading structure is pressing against the fiberglass, the load will cause the fiberglass to be stretched inwards thus resulting in tension. Is this deduction reasonable?
 
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Is that an aluminum frame of sorts breing pressed upward against a fiberglass panel which is supported along its edges only? If so, the fiberglass bending streses are tensile on the outside fibers and compressive on the inside fibers, just like any plate subject to bending loads. Calculating those streses is quite difficult without a copy of Roarke's 'Stress and Strain' or computer finite element software.
 
Hi there,

I do have Roark's. But I am not so sure if it possible to apply those formulas meant for metal plates to my composite? I am quite lost actually. :(
 
Hi there,

I've included a picture of my loading condition. I've realized Roark does not provide any flat plate condition similar to that of my problem but I was wondering if it is possible to use Case no 8 in page 508 of Roark's?

I plan to take the outer dimension minus the inner dimension. Please advise as I am extremely new to structural engineering and I would gladly appreciate if someone could help me.

Thanks!
 

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