BULETINUL INSTITUTULUI POLITEHNIC DIN IAŞI
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102 Iulian Agape et al<br />
were measured in 11 equidistant points (so n=10) on the length L = 1.65 m for<br />
the damaged front. The taken deformations were: ξ 1 = 0.53 m; ξ 2 = 0.52 m; ξ 3 =<br />
= 0.50 m; ξ 4 = 0.43 m; ξ 5 = 0.33 m; ξ 6 = 0.31 m; ξ 7 = 0.27 m; ξ 8 = 0.19 m;<br />
ξ 9 =0.13 m; ξ 10 = 0.14 m; ξ 11 = 0.12 m.<br />
We specify that ξ 1 , ξ 3 , ξ 5 , ξ 7 , ξ 9 , ξ 11 , have the exactly considered values in<br />
the 6 equidistant points from the application (Gaiginschi, 2008). The other 5<br />
considered values for the deformation, in this example, do not distort the<br />
deformation character. The adopted values keep the increase or decrease<br />
deformation character, on the considered intervals.<br />
Table 1 and 2 centralize the calculus results for the m i coefficients and<br />
K 1 , K 2 , K 3 coefficients, the average deformation and deformation energy. The<br />
calculus considered both adopting cases for stiffness coefficients A, B and G,<br />
respectively the ones recommended by SAE, and also the experimentally ones.<br />
Table 1<br />
ξ m<br />
[m] [1/m]<br />
0.53 0<br />
0.52 -0.02029<br />
0.5 -2.1227<br />
0.43 -2.50818<br />
0.33 5.543869<br />
0.31 -2.03644<br />
0.27 -1.80584<br />
0.19 0.444351<br />
0.13 4.436144<br />
0.14 -2.76193<br />
0.12 0<br />
Table 2<br />
k 1 k 2 k 3<br />
Coeficients<br />
m sqm Cubm<br />
0.825 0.519236 0.178861<br />
G, N A, N/m B, N/sqm<br />
exp 13007.42 102481.6 807422.2<br />
sae 2715.543 36200.93 482595<br />
Ed exp, [J] 208359.3<br />
Ed sae, [J] 107354.4<br />
ξmed, [m] 0.315<br />
4. Conclusions<br />
1. Comparing the results with the ones obtained in the application from<br />
(Gaiginschi, 2008), we notice an increase of about 32…37% for the<br />
deformation energy, depending on the adopted coefficients type. On the other