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Failure analyses of composite bolted joints
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pipes, R. B. Wilson, D. W. York, J. L. Gillespie, J. W. |
| Copyright Year | 1980 |
| Description | The complex failure behavior exhibited by bolted joints of graphite epoxy (Hercules AS/3501) was investigated for the net tension, bearing and shearout failure modes using combined analytical and experimental techniques. Plane stress, linear elastic, finite element methods were employed to determine the two dimensional state of stress resulting from a loaded hole in a finite width, semiinfinite strip. The stresses predicted by the finite element method were verified by experiment to lend credence to the analysis. The influence of joint geometric parameters on the state of stress and resultant strength of the joint was also studied. The resulting functional relationships found to exist between bolted joint strength and the geometric parameters, were applied in the formulation of semiempirical strength models for the basic failure modes. A point stress failure criterion was successfully applied as the failure criterion for the net tension and shearout failure modes. |
| File Size | 2641828 |
| Page Count | 80 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810002905 |
| Archival Resource Key | ark:/13960/t03z32r5m |
| Language | English |
| Publisher Date | 1980-07-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Stress Analysis Joints Junctions Failure Modes Bolted Joints Bolts Notch Tests Tensile Strength Specimen Geometry Finite Element Method Plane Stress Failure Analysis Shear Stress Graphite-epoxy Composites Composite Structures Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |