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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

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