The in-plane properties of orthotropic lamina (carbon fiber) are presented as below: E₁= 150 GPa, E = 20 GPa, G₁₂ = 15 G
Posted: Wed May 04, 2022 9:30 am
I am posting for 3rd time no correct answer till now
The in-plane properties of orthotropic lamina (carbon fiber) are presented as below: E₁= 150 GPa, E = 20 GPa, G₁₂ = 15 GPa, P=0.25, an = 6μm/m °C, a₂ = 20 μm/m "C, P = 100 μm/m %M and = 1,200 μm/m %M: a. Determine the state of strains in the coordinate system under applied stress (₁) of 250MPa, hygrothermal loads (AT=80°C and AM=2%). The boundaries are fixed along the X, direction. b. Determine the state of strains in the coordinate system under applied stress (₂2) of 20 MPa and hygrothermal loads (AT= 80°C and AM = 2%). The boundaries are fixed along the X, direction. 20 MPa AT = 80°C Fix AM = 2% 250 MPa Fix 250 MPa Fix Magno CHOMOMON 20 MPa Fix
The in-plane properties of orthotropic lamina (carbon fiber) are presented as below: E₁= 150 GPa, E = 20 GPa, G₁₂ = 15 GPa, P=0.25, an = 6μm/m °C, a₂ = 20 μm/m "C, P = 100 μm/m %M and = 1,200 μm/m %M: a. Determine the state of strains in the coordinate system under applied stress (₁) of 250MPa, hygrothermal loads (AT=80°C and AM=2%). The boundaries are fixed along the X, direction. b. Determine the state of strains in the coordinate system under applied stress (₂2) of 20 MPa and hygrothermal loads (AT= 80°C and AM = 2%). The boundaries are fixed along the X, direction. 20 MPa AT = 80°C Fix AM = 2% 250 MPa Fix 250 MPa Fix Magno CHOMOMON 20 MPa Fix