A. LIMIT STATE OF SHEAR
1. INTRODUCTION
RCC structures are generally subjected three type of shear stresses namely Flexural shear, punching shear and torsional shear. Diagonal tension arises in the section due to the shear forces which results in formation of cracks in concrete as concrete is weak in tension. Hence, limit state of shear must be checked in design of section. Shear reinforcement is provided in the form of vertical stirrup or bent up bars.
Following are the major mechanism in which shear failure takes place:
(i) Diagonal Tension: At the support of simply supported beam, bending stresses are zero and the shear stresses are maximum. Thus, tensile stresses generated along a plane inclined at 45˚ to the horizontal. As concrete is weak in tension, cracks start to develop at an angle of 45˚.
(ii) Flexural Shear: This type of cracks occurs due to large bending moment and small shear force. Cracks are normally inclined at 90˚ to the horizontal.
(iii) Diagonal Compression: This type of failure also takes place along with diagonal tension in heavily reinforced section. It is characterised by crushing of concrete.
NOMINAL SHEAR STRESS
The average shear stress can be calculated using the following formula:
Where,
Vu = ultimate shear stress at the section
b = width of the section
d = effective depth of the section
For beams with varying depth
Where,
β = inclination of flexural tensile force to the horizontal.
Mu = factored bending moment at the section.
Bond, Anchorage and Development Length
Bond stress
Where V = Shear force at any section
d = Effective depth of the section
∑ p = Sum of all perimeter of reinforcement
n = Number of reinforcement
diameter of reinforcement
Permissible bond stress
As per IS 456 : 2000
- These value of bond stress is for plain bar in tension.
- For deformed bar the above value should be increased by 60%.
- For bar in compression the above value should be increased by 25%.
Development Length (Ld)
Shear stress
Shear stress
(a) For Homogeneous beam
where,
q = shear stress at any section
V = shear force at any section
Moment of area of section above the point of consideration
I = Moment of inertia of section
(b) For Reinforced concrete beam
(i) Shear stress above NA
(ii) Shear stress below NA
Nominal shear stress,
Design shear strength of concrete without shear reinforcement as per IS 456: 2000 depends on
(i) Grade of concrete
(ii) Percentage of steel,
Where,
Ast = Area of steel
b = Width of the Beam
d = Effective depth of the beam
Maximum shear stress with shear reinforcement is
Minimum shear reinforcement (As per IS 456 : 2000)
This is valid for both WSM and LSM
where,
ASV = Area of shear reinforcement
SV = Spacing for shear reinforcement
Spacing of shear reinforcement
Maximum spacing is minimum of (i), (ii) and (iii)
(i)
(ii) 300 mm
(iii) 0.75 → For vertical stirrups
d → For inclined stirrups
where, d = effective depth of the section
(a) Critical section X-X at d from the face of the support
(b) Critical section X-X at the face of the support
The above provisions are applicable for beams generally carrying uniformly distributed load or where the principal load is located beyond 2d from the face of the support.
Vertical stirrups:
Shear force VS will be
Resisted by shear Reinforcement provided in 'd' length of the beam,
where, ASV = Cross-sectional area of stirrups
SV = Centre to centre spacing of stirrups
Inclined stirrups: or a series of bars bent-up at different cross-section:
Bent up Bars:
- Single or a group of bent up bars are provided at distance from support.
Generally bar should not be bent up beyond a distance l/4 from the support. Where l = length of span.
B. LIMIT STATE OF TORSION
- INTRODUCTION
In RCC structures generally torsion is accompanied by flexure and shear. It occurs if the line of action of force does not passes through the shear centre. Torsion is divided into two categories:
(i) Primary Torsion: Developed due to eccentric loading.
(ii) Secondary Torsion: Torsion is induced in the structure due to rotation of a member which depends on torsional stiffness of the member.
- DESIGN OF TORSION
Torsion induces shear stress in the member which causes warping of non-circular section. Diagonal tension develops in the section which causes torsional cracking in the section. Torsional strength is improved by providing longitudinal and transverse reinforcement. The longitudinal reinforcement helps in reducing cracks through dowel action while transverse reinforcement helps in resisting shear stresses.
As per IS 456 the effect of torsional stresses is divided into
(i) Equivalent Shear
(ii) Equivalent moment
2.1. Equivalent Shear
Ve = Equivalent shear force
Vu = Shear force
Tu = Torsional moment
B = Width of the section
The equivalent nominal shear stress is calculated by dividing the equivalent shear force divided by area of the section.
2.2. Longitudinal reinforcement
The longitudinal tension reinforcement should be designed to carry equivalent bending moment of
Where,
Mu = Flexural moment
Mt =
Tu = Torsional moment
D = Overall depth of the section
b = width of the section
- If numerical value of Mt exceeds the numerical value of Mu, compression longitudinal reinforcement is provided to resist the bending moment equal to (Mt – Mu).
- The reinforcement should be provided close to the corners.
- If the depth of the section exceeds 450 mm, the area of reinforcement equal to 0.1% of web area should be distributed equally on both faces.
2.3. Transverse Reinforcement
As per Is 456, transverse reinforcement is provided in the form of two legged closed hoops. The area of transverse reinforcement is obtained by the following formula:
Where,
Tu = Torsional moment
Vu = Shear force
sv = Spacing of shear reinforcement
b1 = centre to centre distance between corner bar in the direction of width
d1 = centre to centre distance between corner bar in the direction of depth
b = width of the member
fy = Characteristics strength of stirrup reinforcement
τve = equivalent nominal shear stress
τc = shear strength of concrete
Note: The distribution of transverse reinforcement should be such that the spacing should be a minimum value of x1, or 300 mm where x1 and y1 are short and long dimension of stirrup.
x1 = b1 + Diameter of longitudinal bar + Diameter of stirrup
y1 = d1 + Diameter of longitudinal bar + Diameter of stirrup
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