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area D f BZ,3,I
F u
F u
area D f BZ,3,II
F R,4
D b
BZ
CMOD, Deflection (mm)
Deflection (mm)
3
Fu
CMOD = 3 mm
4
= 3.5 mm
4
0.3
2.35
Fig. 3.10 Equivalent
fl
exural tensile strength (left) and residual
fl
exural tensile strength (right), [ 75 ]
where:
= 2 D f BZ ; 3 ; I . 2
D f BZ ; 3 ; II . 2
L . bh sp
3
f eq ; 3 ¼
65 þ
:
:
5
. 2bh sp
3F R ; 4 L
f R ; 4 ¼
exural tensile strength, it
might be necessary to tune the design formulas. The relation between f eq,I and f R,I
for the
Due to the change from the equivalent to the residual
fl
bers used within the Brite/Euram project is shown in Fig. 3.11 . For shear
design f eq,3 replaced by f R4 , by considering a factor 1/0.87. The relation shown in
Fig. 3.11 depends on the post-cracking behavior of the FRC.
8.0
f R1
f R4
f eq2
f eq3
f R1
=
0.95 +0.48
7.0
f eq2
6.0
5.0
f R4
=
0
f eq3
4.0
3.0
2.0
1.0
0.0
0.0
1.0
2.0
3.0
4.0
5.0
6.0
7.0
8.0
Equivalent flexural tensile strength [MPa]
f eq
Fig. 3.11 Relation between equivalent
fl
exural
tensile strength and residual
fl
exural
tensile
strength for the bers used within the Brite/Euram project [ 75 , 94 ]
 
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