Kethavath Srinath
Osmania University (OU), Hyderabad
Kethavath Srinath has created this Calculator and 300+ more calculators!
Mridul Sharma
Indian Institute of Information Technology (IIIT), Bhopal
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11 Other formulas that you can solve using the same Inputs

Maximum Bearing Pressure when Full Bearing Area of Sq and Rect Footings is Engaged
Maximum Bearing Pressure=(Axial Load/Area of Footing)*(1+(Loading Eccentricity 1*Principal Axis 1/(Radius of Gyration 1^2))+(Loading Eccentricity 2*Principal Axis 2/(Radius of Gyration 2^2))) GO
Neutral Axis to Outermost Fiber Distance when Total Unit Stress in Eccentric Loading is Given
Outermost Fiber Distance=(Total Unit Stress-(Axial Load/Cross sectional area))*Moment of Inertia about Neutral Axis/(Axial Load*Distance_from Load Applied) GO
Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given
Moment of Inertia about Neutral Axis=(Axial Load*Outermost Fiber Distance*Distance_from Load Applied)/(Total Unit Stress-(Axial Load/Cross sectional area)) GO
Total Unit Stress in Eccentric Loading
Total Unit Stress=(Axial Load/Cross sectional area)+(Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis) GO
Maximum Bending Moment when Maximum Stress For Short Beams is Given
Maximum Bending Moment=((Maximum stress at crack tip-(Axial Load/Cross sectional area))*Moment of Inertia)/Distance from the Neutral axis GO
Maximum Stress For Short Beams
Maximum stress at crack tip=(Axial Load/Cross sectional area)+((Maximum Bending Moment*Distance from the Neutral axis)/Moment of Inertia) 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
Total Unit Stress in Eccentric Loading when Radius of Gyration is Given
Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2))) GO
Eccentricity when Deflection in Eccentric Loading is Given
Eccentricity of Loading=(pi*(1-Axial Load/Critical Buckling Load))*Deflection/(4*Axial Load/Critical Buckling Load) GO
Allowable Bearing Pressure when Area of Lowest Column of a Structure is Given
Allowable Bearing Pressure=Axial Load/Area of foundation GO
Area of foundation of the Lowest Column of a Structure
Area of foundation=Axial Load/Allowable Bearing Pressure 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 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
Total Cross-Sectional Area of Tensile Reinforcing
Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam) GO
Area when water flow equation is given
Cross sectional area=water flow/flow velocity GO

Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given Formula

Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis)))
A=P/(f-((P*c*e/I)))
More formulas
Total Unit Stress in Eccentric Loading GO
Neutral Axis to Outermost Fiber Distance when Total Unit Stress in Eccentric Loading is Given GO
Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given GO
Total Unit Stress in Eccentric Loading when Radius of Gyration is Given GO
Eccentricity when Deflection in Eccentric Loading is Given GO

Define Stress?

In continuum mechanics, stress is a physical quantity that expresses the internal forces that neighboring particles of a continuous material exert on each other, while strain is the measure of the deformation of the material.

How to Calculate Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given?

Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given calculator uses Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))) to calculate the Cross sectional area, The Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given formula is defined as the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point. Cross sectional area and is denoted by A symbol.

How to calculate Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given using this online calculator? To use this online calculator for Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given, enter Axial Load (P), Total Unit Stress (f), Outermost Fiber Distance (c), Distance_from Load Applied (e) and Moment of Inertia about Neutral Axis (I) and hit the calculate button. Here is how the Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given calculation can be explained with given input values -> 0.980761 = 98.0664999999931/(100-((98.0664999999931*0.01*0.1/10))).

FAQ

What is Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given?
The Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given formula is defined as the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point and is represented as A=P/(f-((P*c*e/I))) or Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))). Axial Load is defined as applying a force on a structure directly along an axis of the structure, Total Unit Stress is defined as the the total force acting on unit area, Outermost Fiber Distance is defined as the distance in between the Neutral Axis and Outermost Fiber, Distance_from Load Applied is defined as the length from which the load is applied and Moment of Inertia about Neutral Axis is defined as the moment of inertia of the beam about its neutral axis.
How to calculate Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given?
The Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given formula is defined as the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point is calculated using Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))). To calculate Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given, you need Axial Load (P), Total Unit Stress (f), Outermost Fiber Distance (c), Distance_from Load Applied (e) and Moment of Inertia about Neutral Axis (I). With our tool, you need to enter the respective value for Axial Load, Total Unit Stress, Outermost Fiber Distance, Distance_from Load Applied and Moment of Inertia about Neutral Axis 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 Axial Load, Total Unit Stress, Outermost Fiber Distance, Distance_from Load Applied and Moment of Inertia about Neutral Axis. 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=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=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam)
  • 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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