Precast/Prestressed Girder Help

SHEAR DESIGN

Shear design will be carried out at the critical section near the left pier. Transverse shear reinforcement shall be provided when:

V u > 0.5 ϕ ( V c + V p ) LRFD Eq. 5.8.2.4-1

where:

Vu = total factored shear force, kN.

Vc = shear strength provided by concrete, kN.

Vp = component of the effective prestressing force in the direction of the applied shear, kN.

Φ=resistance factor. [LRFD Art. 5.5.4.2.1]

Critical section near the supports is the greater of 0.5 dv cot and dv from the face of the support. [LRFD Art. 5.8.3.2]

where:

dv = Effective shear depth = distance between resultants of tensile and compressive forces, but not less than the greater of 0.9 de and 0.72 h, mm. [LRFD Art. 5.8.2.9]

de = the corresponding effective depth from the extreme compression fiber to the centroid of the tensile force in the tensile reinforcement = 1705 mm.

Note: de is calculated considering the non-prestressed reinforcement in the slab as the main reinforcement and neglecting the prestress reinforcement. This is because this section lies in the negative moment zone.

a = depth of the equivalent compression block = 108 mm

h = total height of the section = 1800 mm

θ = angle of inclination of diagonal compressive stresses, assume = 36.9º

It is obvious that the shear design at any section depends mainly on the angle of diagonal compressive stresses at this section. The shear design is an iterative process that begins with assuming a value for β. In the following example, only the final cycle of calculations are shown:

dv = de - a/2= 1705 - 0.5 (108)= 1651 mm

> 0.9 de= 0.9 (1705)= 1534.5 mm

> 0.72 h= 0.72 (1800)= 1296.0 mm

Therefore, dv= 1651 mm

Critical section near the supports is the greater of 0.5 dv cot θ = 0.5 (1651) cot 36.9 ° = 1099.5 mm and dv = 1655.4 mm. Therefore dv controls.

Since the width of the bearing is not yet determined, it is conservatively assumed to be equal to zero for the computation of the critical section of shear. Therefore, the critical section in shear is at a distance of 300 + 1651 = 1951 mm from the centerline of

the pier. Check that bv satisfies Eq. 5.8.3.3-2:

V u ϕ V n = 0.25 f ` c b v d v + V p LRFD Eq. 5.8.3.3-2
b v V u ϕ V p 0.25 f ` c d v

Where:

Vu = applied factored shear force at the specified section, taken as positive quantity, kN.

Using load combination Strength I:

Vu = 1671.1 kN

Φ= resistance factor = 0.9 [LRFD Art. 5.5.4.2.1]

Vp = Component of the effective force in the direction of the applied shear

= (Force for 4 draped strands)(sin Ψ) where force for 4 strands

= 394.8 m m 2 × 0.75 × 1861.58 M P a ( 1 0.1857 ) = 448853.43 N
Ψ = tan -1 ( 1600 75 75 9810 ) = 8.4
V p = ( 448853.43 1000 ) sin ( 8.4 ) = 65.2 k N

f`c = 45 MPa

dv = 1.651 m

bv = effective web width of the beam = 150 mm.

150 m m ( 1671.1 0.9 65.2 ) × 1000 0.25 × 45 × 1651 = 96.46 m m
  1. 0.5 cot θ = 1 - this convenient simplification is to take the flange force due to shear as Vu - Vp

Compute the factored shear force and bending moment at the critical section for shear according to Strength I load combinations. Note that in determining εx at a particular section, Mu is taken as positive quantity of the moment corresponding to maximum Vu, but not less than Vudv.[LRFD Art. 5.8.3.4.2]

Vu = 1671.1 kN

Mu = - 936.1 kN-m

Vudv = 1671.1 (1.651) = 2758.99 kN-m

That means that Mu<Vudv therefore the value which will be used for computing εx is Vudv

Compute the Strain in the Reinforcement, εx

ε x = M u d v + 0.5 N u + 0.5 ( V u V p ) cot ( θ ) A p s f p o 2 ( E s A s + E p A p s ) LRFD Eq. 5.8.3.4.2-1

where:

Nu = applied factored normal force at the specified section = 0 kN.

fpo=a parameter taken as modulus of elasticity of prestressing tendons multiplied by the locked in difference in strain between the prestressing tendons and the surrounding concrete (ksi). For the usual levels of prestressing, a value of 0.7 fpu will be appropriate for both pretensioned and post tensioned members, MPa.

Within the transfer length, fpo shall be increased linearly from zero at the location where the bond between the strands and concrete commences to its full value at the end of the transfer length.

Compute the C.G. of Prestressing Strands at the Critical Location for Shear:

The c.g. of the 4 draped strands= 75 + 1450 9810 ( 9810 1805 ) = 1258 measured from the bottom fiber of the beam.

The c.g. for all the strands 4 ( 1258 ) + 32 ( 75 ) 36 = 206.44 mm measured from the bottom of the beam. Thus, eccentricity of strand group at critical section of shear is 722 - 206.5 = 515.5 mm.

f p o = 0.7 f p u = 0.7 × 1968.58 = 1303.1 M P a LRFD Art. C5.8.3.4.2

Aps = area of prestressing steel on the flexural tension side of the member. The flexural tension side of the member should be taken the half-depth containing the flexural tension zone as illustrated in LRFD Fig. 5.8.3.4.2-3.=4(98.7)=394.8mm2

As = area of non prestressing steel on the flexural tension side of the member=6531mm2

Vp = 65.2 kN

As per 2003 Interims, Art. 5.8.3.4.2:

  1. 0.5 cot θ = 1 - this convenient simplification is to take the flange force due to shear as Vu - Vp
  2. the initial value of εx should not taken greater than 0.001.

Therefore,

ε x = M u d v + 0.5 N u + ( V u V p ) cot ( θ ) A p s f p o 2 ( E s A s + E p A p s ) = 2758.99 ( 10 6 ) + ( 1671.1 65.2 ) 10 3 394.8 ( 1303.1 ) 2 ( 207000 ( 6531 ) + 197000 ( 394.8 ) ) = 9.79 × 10 4 0.001
V u = V u ϕ V p ϕ b v d v

where:

Vu= factored shear stress on the concrete, MPa.

bv = Effective web width of the beam= 150 mm.

V u = 71 × 10 3 0.9 ( 652 ( 56.8 ) × 10 3 ) ( 0.9 ) ( 150 ) ( 1651 ) = 7.234 M P a
( V u / f ` c ) = 7.234 45 = 0.161

From LRFD Fig. 5.8.3.4.2-1, using linear interpolation, are obtained the values for θ and β using (vu/f`c ) and εx.

Therefore θ = 36.9° and β= 2.04

where:

β=factor indicating ability of diagonally cracked concrete to transmit tension (a value indicating concrete contribution).[LRFD Art. 5.8.3.4]

Shear Force Carried by the Concrete:

V c = 0.083 β f ` b v d v = 0.083 × 2.04 × 45 × 150 × 1651 10 3 = 281.4 k N LRFD Eq. 5.8.3.3-3

Check if V u > 0.5 ϕ ( V c + V p )

V u = 1671.1 k N > 0.5 ϕ ( V c + V p ) = 0.5 × 0.9 × ( 281.4 + 65.2 ) = 155.97 k N

Therefore, transverse shear reinforcement is required.

V n = ( V u / ϕ ) V c + V s + V p LRFD Eq. 5.8.3.3-1

Where:

Vs = shear force carried by transverse reinforcement

= ( V u / ϕ ) V c V p = 1671.1 0.9 281.4 65.2 = 1510.1 k N
= A v f y d v ( cot ( θ ) + cot ( α ) ) sin ( α ) S LRFD Eq. 5.8.3.3-4

where:

Av = area of shear reinforcement within a distance s, mm2.

s = spacing of stirrups, mm.

fy = yield strength of shear reinforcement, MPa.

α= angle of inclination of transverse reinforcement to longitudinal axis = 90º.

Therefore, required area of shear reinforcement within a spacing s is:

A v / s = V s f y d v cot ( θ ) = 1510.1 × 10 3 413.7 × 1651 × cot ( 36.9 deg ) = 1.6602 m m 2 / m

Check Minimum Reinforcement Required:

The area of minimum transverse reinforcement should satisfy the following equation:

A v 0.083 f ` c b v s f y LRFD Eq. 5.8.2.5-1
M i n i m u m ( A v / s ) = 0.083 45 150 413.7 = 0.20189 m m 2 / m m

Thus, minimum shear reinforcement does not control.

Check Maximum Spacing of Transverse Reinforcement [LRFD Art. 5.8.2.7]:

Check if

V u < 0.125 f ` c LRFD Eq. 5.8.2.7.-1

or

V u 0.125 f ` c LRFD Eq. 5.8.2.7.-2

where:

0.125 f`c = 0.125 (45) = 5.625 MPa

vu = 7.234 MPa

Since vu > 0.125 f`c,

then S max = 0.4 d v = 0.4 × 1651 = 660.4 m m > 300 m m

Therefore, maximum spacing of the stirrups = 300 mm.