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Backout factors
- Thread starter no2metal
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SWComposites
Aerospace
Which property? stiffness? strength?
To get UD E1, you will need data for E2 (or make an extimate), then use laminate theory to back calculate E1 from Ex of the 0/90 laminate
For UD tensile strength, calculate the P/AE strain for the 0/90 laminate, then multiply the strain times the UD E1 to get UD tensile strength.
To get UD E1, you will need data for E2 (or make an extimate), then use laminate theory to back calculate E1 from Ex of the 0/90 laminate
For UD tensile strength, calculate the P/AE strain for the 0/90 laminate, then multiply the strain times the UD E1 to get UD tensile strength.
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