jmurphy82
Aerospace
- Jun 20, 2007
- 1
This is my first laminate build up and im having trouble determing if i have the right values or where i can get the right values to enter for my skin ply mat card. Im working with an E-761-4581 Quartz prepreg, glass reinforced ply with the following data available.
Tesile Strength
Tesile Modulus
Compressive Modulus
Compressive Strength
Flexural Strength
Flexural Modulus
Short Beam Shear
From what ive found out, i need two Young Modulus', three Shear Modulus', and a poissons ratio, none of which i believe i have. Any help on where i could get these values would be helpful.
Tesile Strength
Tesile Modulus
Compressive Modulus
Compressive Strength
Flexural Strength
Flexural Modulus
Short Beam Shear
From what ive found out, i need two Young Modulus', three Shear Modulus', and a poissons ratio, none of which i believe i have. Any help on where i could get these values would be helpful.