Issue 54

T. I. J. Brito et alii, Frattura ed Integrità Strutturale, 54 (2020) 1-20; DOI: 10.3221/IGF-ESIS.54.01

2 U M M  2 upper b

q

exp

M

i

 

M  

0

(36)

r

d

i

0  

d

i

r

i

Figure 6: Bending Moment vs. Damage response

The following equation shows the result obtained:

 

 

2 2 M U q M  r

b

ln   

(37)

 

upper

2

i

The lower-limit for γ is obtained by the following criterion:

2

U M

b

r

2

d

M

i

i

0   

0

(38)

1

M

 

 

2 exp Y

q

i d

0  

lower

0

i

exp

lower

which leads to:

lower   

(39)

Despite γ lower , when γ values are negative occurs numerical instabilities in the analysis process, leading to values of ultimate damage and plastic damage tending to zero. Therefore, from now on, only positive values for γ are adopted in this paper. Meneghetti [44] A simply supported experimental beam under a four point bending test was carried out by Meneghetti et al. [44], which has as cross section dimensions 15 cm x 30 cm, total length 300 cm and distance between supports 285 cm. For the design due to bending were defined two longitudinal lower bars with 12.5 mm diameter, 317 cm total length and 10 cm anchorage at each edge; two longitudinal upper bars with 6.3 mm diameter, 297 cm total length. For the design due to shearing were calculated 42 stirrups with 6.3 mm diameter, 7 cm spacing, 90 cm total length and 6cm anchorage at each tip and the covering adopted was 15 mm (see Fig. 7). Results of strength limits, 6.3 mm steel bars acquired the followed magnitude tensions, 508 MPa and 713 MPa, yield and rupture, respectively. 12.5 mm bars acquired yield tension value 578 MPa and

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