Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given Calculator

Category	Engineering ↺
Engineering	Civil ↺
Civil	Concrete ↺
Concrete	Working Stress Design of Tension Reinforced Rectangular Beams ↺
Working-Stress-Design-Of-Tension-Reinforced-Rectangular-Beams	Allowable Shear ↺

✖excess shear is the v' = V - Vc* bdⓘ excess shear [V']			+10% -10%
✖Stirrup Spacing is the approximate minimum spacing between two bars in a section.ⓘ Stirrup Spacing [s]			+10% -10%
✖Stirrup Area (Av) is the total cross-sectional area of the stirrup bars used.ⓘ Stirrup Area [Av]			+10% -10%
✖Distance from Compression to Centroid Reinforcment is defined as the distance from extreme compression surface to the centroid of compression reinforcement, in (mm).ⓘ Distance from Compression to Centroid Reinforcment [d']			+10% -10%

✖Allowable stress in stirrup steel is 55% of those for ultimate strength design.ⓘ Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given [f_v]

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Ishita Goyal

Meerut Institute of Engineering and Technology (MIET), Meerut

Ishita Goyal has created this Calculator and 100+ more calculators!

Himanshi Sharma

Bhilai Institute of Technology (BIT), Raipur

Himanshi Sharma has verified this Calculator and 500+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Ultimate Strength for Symmetrical Reinforcement

Axial Load Capacity=0.85*28 Day Compressive Strength of Concrete*Width of compression face*Distance from Compression to Tensile Reinforcement*Capacity reduction factor*((-Area ratio of tensile reinforcement)+1-(Eccentricity by method of frame analysis/Distance from Compression to Tensile Reinforcement)+sqrt(((1-(Eccentricity by method of frame analysis/Distance from Compression to Tensile Reinforcement))^2)+2*Area ratio of tensile reinforcement*((Force ratio of strengths of reinforcements-1)*(1-(Distance from Compression to Centroid Reinforcment/Distance from Compression to Tensile Reinforcement))+(Eccentricity by method of frame analysis/Distance from Compression to Tensile Reinforcement)))) GO

Balanced Moment when Φ is Given

Balanced Moment=Resistance Factor*((.85*28 Day Compressive Strength of Concrete*Width of compression face*Depth Rectangular Compressive Stress*(Distance from Compression to Tensile Reinforcement-Distance from Plastic to Tensile Reinforcement-Depth Rectangular Compressive Stress/2))+(Area of Compressive Reinforcement*Yeild Strength of Base Plate*(Distance from Compression to Tensile Reinforcement-Distance from Compression to Centroid Reinforcment-Distance from Plastic to Tensile Reinforcement))+(area of tension reinforcement*Tensile Stress in Steel*Distance from Plastic to Tensile Reinforcement)) GO

Ultimate Strength for Symmetrical Reinforcement in Single Layers

Axial Load Capacity=Capacity reduction factor*((Area of Compressive Reinforcement*Yield strength of reinforcing steel/((Eccentricity/Distance from Compression to Tensile Reinforcement)-Distance from Compression to Centroid Reinforcment+0.5))+(Width of compression face*Depth of column*28 Day Compressive Strength of Concrete/((3*Depth of column*Eccentricity/(Distance from Compression to Tensile Reinforcement^2))+1.18))) GO

Stirrup Spacing for Practical Design

Spacing of Stirrups=(Stirrup Area*Capacity reduction factor*Yield strength of reinforcing steel*Effective depth of beam)/((Design Shear )-((2*Capacity reduction factor)*sqrt(28 Day Compressive Strength of Concrete)*Breadth of the web*Effective depth of beam)) GO

Reinforcement Yield Strength when Axial Load for Tied Columns is Given

yield strength of reinforcement=(Bending moment)/(0.40*area of tension reinforcement*(Distance from Compression to Tensile Reinforcement-Distance from Compression to Centroid Reinforcment)) GO

Tension Reinforcement Area when Axial Load for Tied Columns is Given

area of tension reinforcement=(Bending moment)/(0.40*yield strength of reinforcement*(Distance from Compression to Tensile Reinforcement-Distance from Compression to Centroid Reinforcment)) GO

Axial Load for Tied Columns

Bending moment=0.40*area of tension reinforcement*yield strength of reinforcement*(Distance from Compression to Tensile Reinforcement-Distance from Compression to Centroid Reinforcment) GO

Nominal Reinforcement Shear Strength when Area of Steel in Vertical Stirrups is Given

Nominal shear strength by reinforcement=(Area of steel required*yield strength of reinforcement*Centroidal distance of tension reinforcement)/(Stirrup Spacing) GO

Area of Steel Required in Vertical Stirrups

Area of steel required=(Nominal shear strength by reinforcement*Stirrup Spacing)/(yield strength of reinforcement*Centroidal distance of tension reinforcement) GO

Nominal Reinforcement Shear Strength when Stirrup Area with Support Angle is Given

Nominal strength of Shear Reinforcement=(Stirrup Area)/(Yield strength of reinforcing steel)*sin(Angle at Support) GO

Shear Reinforcement Yield Strength when Stirrup Area with Support Angle is Given

yield strength of reinforcement=(Strength of Shear Reinforcement)/((Stirrup Area)*sin(Angle at Support)) GO

Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given Formula

allowable stress in stirrup steel=(excess shear*Stirrup Spacing)/(Stirrup Area*Distance from Compression to Centroid Reinforcment)
f<sub>v=(V'*s)/(Av*d')

More formulas

Nominal Unit Shear Stress GO

Shear when Nominal Unit Shear Stress is Given GO

Distance from Extreme Compression to Centroid when Nominal Unit Shear Stress is Given GO

Beam Width when Nominal Unit Shear Stress is Given GO

Area Required in Legs of a Vertical Stirrup GO

Excess Shear when Area in Legs of a Vertical Stirrup is Given GO

Stirrups Spacing when Area in Legs of a Vertical Stirrup is Given GO

Distance from Extreme Compression to Centroid when Area in Legs of a Vertical Stirrup is Given GO

Stirrups Spacing when Stirrup Leg Area is Given for Group of Bars Bent up Different Distances GO

Excess Shear when Stirrup Leg Area is Given for Group of Bars Bent up Different Distances GO

Vertical Stirrup Leg Area when Group of Bars is Bent at Different Distances GO

Excess Shear when Vertical Stirrup Leg Area is Given for Single Bar Bent at Angle α GO

Vertical Stirrup Leg Area when Single Bar is Bent at an Angle α GO

What is stirrup?

Stirrup is a closed loop of reinforcement bar, which has the main function of holding the main reinforcement bars together in a reinforced concrete element.

How to Calculate Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given?

Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given calculator uses allowable stress in stirrup steel=(excess shear*Stirrup Spacing)/(Stirrup Area*Distance from Compression to Centroid Reinforcment) to calculate the allowable stress in stirrup steel, Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given formula is defined as the maximum stress that is allowed to be applied on a vertical stirrup. allowable stress in stirrup steel and is denoted by f_v symbol.

How to calculate Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given using this online calculator? To use this online calculator for Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given, enter excess shear (V'), Stirrup Spacing (s), Stirrup Area (Av) and Distance from Compression to Centroid Reinforcment (d') and hit the calculate button. Here is how the Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given calculation can be explained with given input values -> 0.1 = (1*0.05)/(5E-05*0.01).

FAQ

What is Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given?

Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given formula is defined as the maximum stress that is allowed to be applied on a vertical stirrup and is represented as f_{v=(V'*s)/(Av*d')} or allowable stress in stirrup steel=(excess shear*Stirrup Spacing)/(Stirrup Area*Distance from Compression to Centroid Reinforcment). excess shear is the v' = V - Vc* bd, Stirrup Spacing is the approximate minimum spacing between two bars in a section, Stirrup Area (Av) is the total cross-sectional area of the stirrup bars used and Distance from Compression to Centroid Reinforcment is defined as the distance from extreme compression surface to the centroid of compression reinforcement, in (mm).

How to calculate Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given?

Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given formula is defined as the maximum stress that is allowed to be applied on a vertical stirrup is calculated using allowable stress in stirrup steel=(excess shear*Stirrup Spacing)/(Stirrup Area*Distance from Compression to Centroid Reinforcment). To calculate Allowable Stress in Stirrup Steel when Area in Legs of a Vertical Stirrup is Given, you need excess shear (V'), Stirrup Spacing (s), Stirrup Area (Av) and Distance from Compression to Centroid Reinforcment (d'). With our tool, you need to enter the respective value for excess shear, Stirrup Spacing, Stirrup Area and Distance from Compression to Centroid Reinforcment and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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