Total Unit Stress in Eccentric Loading Calculator

Category	Engineering ↺
Engineering	Civil ↺
Civil	Beams ↺
Beams	Eccentric Loading ↺

✖Axial Load is defined as applying a force on a structure directly along an axis of the structureⓘ Axial Load [P]			+10% -10%
✖Cross sectional area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specifies axis at a point.ⓘ Cross sectional area [A]			+10% -10%
✖Outermost Fiber Distance is defined as the distance in between the Neutral Axis and Outermost Fiberⓘ Outermost Fiber Distance [c]			+10% -10%
✖Distance_from Load Applied is defined as the length from which the load is applied.ⓘ Distance_from Load Applied [e]			+10% -10%
✖Moment of Inertia about Neutral Axis is defined as the moment of inertia of the beam about its neutral axisⓘ Moment of Inertia about Neutral Axis [I]			+10% -10%

✖Total Unit Stress is defined as the the total force acting on unit area.ⓘ Total Unit Stress in Eccentric Loading [f]

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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

Stress at Point y for a Curved Beam

Stress=((Bending Moment )/(Cross sectional area*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

Bending Moment When Stress is Applied at Point y in a Curved Beam

Bending Moment =((Stress*Cross sectional area*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 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

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

Axial Load when Maximum Stress For Short Beams is Given

Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO

Electric Current when Drift Velocity is Given

Electric Current=Number of free charge particles per unit volume*[Charge-e]*Cross sectional area*Drift Velocity GO

Resistance

Resistance=(Resistivity*Length of Conductor)/Cross sectional area GO

Centrifugal Stress

Centrifugal Stress=2*Tensile Stress*Cross sectional area GO

Rate of Flow

Rate of flow=Cross sectional area*Average Velocity GO

< 1 Other formulas that calculate the same Output

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

Total Unit Stress in Eccentric Loading Formula

Total Unit Stress=(Axial Load/Cross sectional area)+(Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis)
f=(P/A)+(P*c*e/I)

More formulas

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

When the load acting on the column is offset from the centroid of the column, then it establishes the bending of the column along with the axial stress. This offset loading of the column is referred to as eccentric loading.

How to Calculate Total Unit Stress in Eccentric Loading?

Total Unit Stress in Eccentric Loading calculator uses Total Unit Stress=(Axial Load/Cross sectional area)+(Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis) to calculate the Total Unit Stress, The Total Unit Stress in Eccentric Loading formula is defined as the total force applied on a unit area. Total Unit Stress and is denoted by f symbol.

How to calculate Total Unit Stress in Eccentric Loading using this online calculator? To use this online calculator for Total Unit Stress in Eccentric Loading, enter Axial Load (P), Cross sectional area (A), 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 Total Unit Stress in Eccentric Loading calculation can be explained with given input values -> 9.816457 = (98.0664999999931/10)+(98.0664999999931*0.01*0.1/10).

FAQ

What is Total Unit Stress in Eccentric Loading?

The Total Unit Stress in Eccentric Loading formula is defined as the total force applied on a unit area and is represented as f=(P/A)+(P*c*e/I) or Total Unit Stress=(Axial Load/Cross sectional area)+(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, Cross sectional area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specifies axis at a point, 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 Total Unit Stress in Eccentric Loading?

The Total Unit Stress in Eccentric Loading formula is defined as the total force applied on a unit area is calculated using Total Unit Stress=(Axial Load/Cross sectional area)+(Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis). To calculate Total Unit Stress in Eccentric Loading, you need Axial Load (P), Cross sectional area (A), 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, Cross sectional area, 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 Total Unit Stress?

In this formula, Total Unit Stress uses Axial Load, Cross sectional area, Outermost Fiber Distance, Distance_from Load Applied and Moment of Inertia about Neutral Axis. We can use 1 other way(s) to calculate the same, which is/are as follows -

Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2)))

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