Compression or Tensile on Fiberglass

AI Thread Summary
The discussion focuses on the effects of compressive forces applied to fiberglass material by an aluminum structure. It highlights the tensile and compressive stresses experienced by the fiberglass due to bending, with tensile strength values provided for both the warp and weft layers of the fiberglass. The user expresses uncertainty about applying metal plate stress formulas from Roark's to composite materials and seeks guidance on calculating stresses in their specific loading condition. They are particularly interested in whether a specific case from Roark's can be adapted for their scenario. Overall, the conversation emphasizes the complexities of analyzing composite materials under load.
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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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