PSI - Issue 11
R. Capozucca et al. / Procedia Structural Integrity 11 (2018) 402–409
408
7
R. Capozuc
ca, E. Magagnin
/ Structural Inte
grity Procedia 0
0 (2018) 000–000
i, M.V. Vecchietti
Table
4. Exp. results f
L P or strengthened R oad [kN] Defle midsp [mm]
C beam B2 at da ction at an
mage degrees D at ressive ete ε c
i .
Strain comp concr (10 3 0.10 )
Curvature χ [mm -1 ·10 -5 ]
Strain at steel (intrados) ε s
Damage degrees
(10 -6 ) -0.08 -0.94 -1.90 -7.37 -
D* 1 D* 2 D* 3 D* 4 D* 5
4
.00
0.61 2.83 8.65
0.33 1.51 3.31 10.00 -
8.00
0.31 0.72 1.4 -
16.00
2 3
8.00 7.35
17.00 62.25
T for t again conc
he beam was he different d observe the rete cracking
analysed und amage degre shift of the d damage.
er vibration a e, at each poi iagrams at va
t every damag nt of the acce rious steps D
e step in the lerometer, ar i with reducti
free-free edge e shown for B on of the freq
condition. Th 1 in Figure uency values
e FRF envel 9. It is possib due to incre
opes, le to asing
Fig.8. Crackin
g state of beam B
2 at steps of stat
ic damage D 4 *.
Table
5. Exp. average
frequency values Damage degree
for r = 1,2,3 mo f 1 [Hz] 121 121.17 112 106.33 93,5 ariation valu t the unloade * and D 4 *, c caused by th st load level ow load steps
des of damaged R Δf 1 /f Di* (%) f [
C beam B2.
/f Di*
Δf 3 /f D (%)
Δf 2 (%)
f 3 [Hz]
2 Hz]
i*
-
3 3 3 2 2
33.14 33.67 19.33 92.33
-
631.2 629.2 604. 566.2 524,2
5 5
-
D 0 * D 1 * D 2 * D 3 * D 4 *
0 8 5
0 4 8 4
0 4 6 7
88
5 5
12
80,5
In with at th vibra conc varia
Figure 10 th the initial va e high dama tion mode. T rete cracking tions are also
e frequency v lue recorded a ge levels, D 3 his result is at the lowe recorded at l
es in referenc d condition D ause the grea e presence o s. In the cas that trigger th
e to the differ 0* for B2. It test frequenc f the strength e of unreinf e concrete cr
ent damage d is possible to y’s variation, ening that a orced beams acking.
egree by bend notice how th up to 50%, llows to decr without FRP
ing are comp e load increm in the fist na ease the effe rod, the hi
ared ents tural ct of ghest
1
0,1
0,01
0,001
lg
0,0001
MODE II D 0 *
MO D 0 *
DE IV
200 MODE D 0 *
I
600 80 requency [Hz MODE D 0 *
III
0,00001
0
400
0 1000 ]
F
Fi
g.9. Envelope of
FRFs for differen
t damage degree
, D* I , for beam B 2.
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