Kethavath Srinath
Osmania University (OU), Hyderabad
Kethavath Srinath has created this Calculator and 400+ more calculators!
Mridul Sharma
Indian Institute of Information Technology (IIIT), Bhopal
Mridul Sharma has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Deflection for Hollow Rectangle When Load in Middle
Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*(Sectional Area*(Depth of the Beam^2)-Interior Cross-Sectional Area of Beam*(Interior Depth of the Beam^2))) GO
Deflection for Hollow Rectangle When Load is Distributed
Deflection of Beam=Greatest Safe Load*(Length of the Beam^3)/(52*(Sectional Area*Depth of the Beam^-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam^2)) GO
Greatest Safe Load for Hollow Rectangle When Load is Distributed
Greatest Safe Load=1780*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam)/Distance between Supports GO
Greatest Safe Load for Hollow Rectangle When Load in Middle
Greatest Safe Load=(890*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam))/Length of the Beam GO
Deflection for Solid Rectangle When Load is Distributed
Deflection of Beam=(Greatest safe distributed load*Length of the Beam^3)/(52*Sectional Area*Depth of the Beam^2) GO
Deflection for Solid Rectangle When Load in Middle
Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*Sectional Area*Depth of the Beam^2) GO
Strain Energy if moment value is given
Strain Energy=(Bending moment*Bending moment*Length)/(2*Elastic Modulus*Moment of Inertia) GO
Greatest Safe Load for Solid Rectangle When Load is Distributed
Greatest safe distributed load=1780*Sectional Area*Depth of the Beam/Length of the Beam GO
Greatest Safe Load for Solid Cylinder When Load is Distributed
Greatest Safe Load=1333*(Sectional Area*Depth of the Beam)/Length of the Beam GO
Greatest Safe Load for Solid Cylinder When Load in Middle
Greatest Safe Load=(667*Sectional Area*Depth of the Beam)/Length of the Beam GO
Greatest Safe Load for Solid Rectangle When Load in Middle
Greatest Safe Load=890*Sectional Area*Depth of the Beam/Length of the Beam GO

11 Other formulas that calculate the same Output

Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam
Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis)))) GO
Cross-Sectional Area when Axial Buckling Load for a Warped Section is Given
Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2))) GO
Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given
Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))) GO
Cross-sectional area of the rod if stress induced in rod due to impact load is known
Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2)) GO
Cross-Sectional Area when Elastic Critical Buckling Load is Given
Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus) GO
Cross-Sectional Area when Maximum Stress For Short Beams is Given
Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO
Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given
Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity) GO
Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given
Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant) GO
Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given
Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus) GO
Cross-sectional Area of Soil Conveying Flow when Rate of Flow of Water is Given
Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient)) GO
Area when water flow equation is given
Cross sectional area=water flow/flow velocity GO

Total Cross-Sectional Area of Tensile Reinforcing Formula

Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam)
A=8*M/(7*f<sub>s*D)
More formulas
Stress in Concrete GO
Bending Moment when Stress in Concrete is Given GO
Width of Beam when Stress in Concrete is Given GO
Depth of Beam when Stress in Concrete is Given GO
Stress in Steel When Cross-Sectional Reinforcing Tensile Area to Beam Area Ratio is Given GO
Stress in Steel GO
Depth of Roof and Floor Slabs GO
Depth of Light Beams GO
Depth of Heavy Beams and Girders GO
Bending Moment when Total Cross-Sectional Area of Tensile Reinforcing is Given GO
Cross-Sectional Area of Compressive Reinforcing GO
Bending Moment when Cross-Sectional Area of Compressive Reinforcing is Given GO
Moment of Inertia of Transformed Beam Section GO
Distance from Neutral Axis to Tensile Reinforcing Steel when Unit Stress is Given GO
Unit Stress in Tensile Reinforcing Steel GO
Total Bending Moment when Unit Stress in Tensile Reinforcing Steel is Given GO
Moment of Inertia when Unit Stress in Tensile Reinforcing Steel is Given GO
Distance from Neutral Axis to Compressive Reinforcing Steel when Unit Stress is Given GO
Moment of Inertia when Unit Stress in Compressive Reinforcing Steel is Given GO
Total Bending Moment when Unit Stress in Compressive Reinforcing Steel is Given GO
Unit Stress in Compressive Reinforcing Steel GO
Moment of Inertia when Unit Stress in Extreme Fiber of Concrete is Given GO
Distance from Neutral Axis to Face of Concrete when Unit Stress is Given GO
Total Bending Moment when Unit Stress in Extreme Fiber of Concrete is Given GO
Unit Stress in Extreme Fiber of Concrete GO
Shearing Unit Stress in a Reinforced Concrete Beam GO
Total Shear when Shearing Unit Stress in a Reinforced Concrete Beam is Given GO
Width of Beam when Shearing Unit Stress in a Reinforced Concrete Beam is Given GO
Effective Depth of Beam when Shearing Unit Stress in a Reinforced Concrete Beam is Given GO
Cross-Sectional Area of Web Reinforcement GO
Total Shear when Cross-Sectional Area of Web Reinforcement is Given GO
Shear Carried by Concrete when Cross-Sectional Area of Web Reinforcement is Given GO
Effective Depth when Cross-Sectional Area of Web Reinforcement is Given GO
Stirrups Spacing when Cross-Sectional Area of Web Reinforcement is Given GO
Bond Stress on Bar Surface GO
Total Shear when Bond Stress on Bar Surface is Given GO
Beam Effective Depth when Bond Stress on Bar Surface is Given GO
Tensile Reinforcing Bars Perimeters Sum when Bond Stress on Bar Surface is Given GO

Define Tensile Reinforcing?

Reinforced concrete (RC), also called reinforced cement concrete (RCC), is a composite material in which concrete's relatively low tensile strength and ductility are compensated for by the inclusion of reinforcement having higher tensile strength or ductility. The reinforcement is usually, though not necessarily, steel bars (rebar) and is usually embedded passively in the concrete before the concrete sets.

How to Calculate Total Cross-Sectional Area of Tensile Reinforcing?

Total Cross-Sectional Area of Tensile Reinforcing calculator uses Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam) to calculate the Cross sectional area, The Total Cross-Sectional Area of Tensile Reinforcing formula is defined as force per unit area that the force acts upon. Thus, Stresses are either tensile or compressive. Structural materials are chosen by their ability to resist tensile or compressive forces, depending upon the application. Cross sectional area and is denoted by A symbol.

How to calculate Total Cross-Sectional Area of Tensile Reinforcing using this online calculator? To use this online calculator for Total Cross-Sectional Area of Tensile Reinforcing, enter Bending moment (M), Reinforcement Stress (fs) and Depth of the Beam (D) and hit the calculate button. Here is how the Total Cross-Sectional Area of Tensile Reinforcing calculation can be explained with given input values -> 2.250E-6 = 8*50/(7*100000000*0.254000000001016).

FAQ

What is Total Cross-Sectional Area of Tensile Reinforcing?
The Total Cross-Sectional Area of Tensile Reinforcing formula is defined as force per unit area that the force acts upon. Thus, Stresses are either tensile or compressive. Structural materials are chosen by their ability to resist tensile or compressive forces, depending upon the application and is represented as A=8*M/(7*fs*D) or Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam). The Bending moment is the reaction induced in a structural element when an external force or moment is applied to the element, causing the element to bend, Reinforcement Stress as force per unit area that the force acts upon. and Depth of the Beam is the overall depth of the cross section of the beam perpendicular to the axis of the beam.
How to calculate Total Cross-Sectional Area of Tensile Reinforcing?
The Total Cross-Sectional Area of Tensile Reinforcing formula is defined as force per unit area that the force acts upon. Thus, Stresses are either tensile or compressive. Structural materials are chosen by their ability to resist tensile or compressive forces, depending upon the application is calculated using Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam). To calculate Total Cross-Sectional Area of Tensile Reinforcing, you need Bending moment (M), Reinforcement Stress (fs) and Depth of the Beam (D). With our tool, you need to enter the respective value for Bending moment, Reinforcement Stress and Depth of the Beam and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Cross sectional area?
In this formula, Cross sectional area uses Bending moment, Reinforcement Stress and Depth of the Beam. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis))))
  • Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia))
  • Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis)))
  • Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus)
  • Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus)
  • Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant)
  • Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2)))
  • Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity)
  • Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2))
  • Cross sectional area=water flow/flow velocity
  • Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient))
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