Table 3 Related parameters of the analytical model for tensile strength of crimping assembly.
From: Mathematical model for the tensile strength of the crimping assembly of aviation wiring harness end
\({r}_{1}\)(mm) | t (mm) | \({r}_{3}\)(mm) | R (mm) | φ (°) | ν | E (MPa) |
|---|---|---|---|---|---|---|
0.5 | 0.32 | 0.075 | 0.89 | 30 | 0.326 | \(5\times {10}^{4}\) |
μ | K (MPa) | a | n | A | H | \(-\frac{1}{e}\frac{dE*}{de}\) |
0.37 | 98 | 1.28 | 0.46 | 0.893 | 3.1136 | 2.1408 |
