Fastener Analysis
Bolted Joint Stress Field Model
Perform rigorous failure analysis of composite bolted joints using Lekhnitskii's anisotropic elasticity solutions and characteristic distance max strain failure criteria.
Active Laminate
0 plies • 0.0000" thick
Calculated A-Matrix [lb/in]
| 1 (x) | 2 (y) | 6 (xy) | |
|---|---|---|---|
| 1 | 0 | 0 | 0 |
| 2 | 0 | 0 | 0 |
| 6 | 0 | 0 | 0 |
Joint Configuration
Geometry
Applied Loads
Critical Load Type
Select the primary bypass load direction to determine which allowables (tension vs compression) are evaluated.
P(0°)
P(90°)
mech =
thm =
mech
thm
N_by-x =
N_by-y =
N_by-xy =
Angles(°) =
Mx
My
Mxy
Input Data Summary
Plate_thickns =0.000
Kh =1.000
1/Kcs =1.000
Ult. Bearing P =623.6
P Angle =3.5
σ_brg =24943585
σ_brg_BJSFM =24943585
σ_by_x_BJSFM =-1050000
σ_by_y_BJSFM =0
σ_by_xy_BJSFM =0
By-pass Angle =0
Kcomp (Composi-lok) =1.000