Bolt Analysis

3D Bolt Group

Input your fastener locations and applied loads to calculate the forces distributed to each bolt.

1
Attachment Locations

Fastener Stiffness ModelChoose between finite stiffness springs or uniform rigid constraints
Attach #X (in/mm)Y (in/mm)Z (in/mm)Dist (Res)KXKYKZ
1
38.284
2
38.284
3
34.641

2
Applied Loads

Load Stiffness ModelChoose between finite stiffness springs or uniform rigid constraints for load connections
Load #XYZFXFYFZMXMYMZKLXKLYKLZ
1
Totals200.0000.0000.0000.0000.0000.000
Resultant|F| = 200.000|M| = 0.000

Reaction Loads

Attach #PXPYPZXY ShearXZ ShearYZ ShearLoad (Res)
1
-76.120-11.174194.19176.936208.577194.512208.876
2
80.998-11.17446.53281.76593.41247.85494.078
3
195.12222.347-240.722196.398309.871241.757310.676
Totals200.0000.0000.000|F| = 200.000

Group Centroid

X: -2.667
Y: 6.667
Z: 6.667

Total Applied Forces

FX: 200.000 | FY: 0.000 | FZ: 0.000
MX: 0.000 | MY: 12087.000 | MZ: 2455.800

Shared Laminate Builder

Laminate Properties

Input Allowables Format

Toggle between Strain (με) and Stress (ksi). Values in the stack and limits will convert on-the-fly.

NameET1 (Msi)EC1 (Msi)ET2 (Msi)EC2 (Msi)G12 (Msi)ν12t (in)σ₁t (ksi)σ₁c (ksi)σ₂t (ksi)σ₂c (ksi)σ₁₂s (ksi)r_c Tens (in)r_c Comp (in)K_br TensK_br Comp
Save as Custom Preset

Save the current material properties under a name so you can reuse them without re-entering values.

Quick Add Ply Angle
Bulk Add Plies
@
Ply Stack 0 plies
Use the quick-add buttons above to build your layup stack.
Total Thickness:0 in