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
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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
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
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
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

Eccentricity when Deflection in Eccentric Loading is Given Formula

Eccentricity of Loading=(pi*(1-Axial Load/Critical Buckling Load))*Deflection/(4*Axial Load/Critical Buckling Load)
e=(pi*(1-P/P<sub>c))*𝜕 /(4*P/P<sub>c)
More formulas
Total Unit Stress in Eccentric Loading GO
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

Define Eccentric loading?

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

How to Calculate Eccentricity when Deflection in Eccentric Loading is Given?

Eccentricity when Deflection in Eccentric Loading is Given calculator uses Eccentricity of Loading=(pi*(1-Axial Load/Critical Buckling Load))*Deflection/(4*Axial Load/Critical Buckling Load) to calculate the Eccentricity of Loading, The Outermost Fiber Distance when Deflection in Eccentric Loading is Given formula is defined as the distance in between the Neutral Axis and Outermost Fiber. Eccentricity of Loading and is denoted by e symbol.

How to calculate Eccentricity when Deflection in Eccentric Loading is Given using this online calculator? To use this online calculator for Eccentricity when Deflection in Eccentric Loading is Given, enter Axial Load (P), Critical Buckling Load (Pc) and Deflection (𝜕 ) and hit the calculate button. Here is how the Eccentricity when Deflection in Eccentric Loading is Given calculation can be explained with given input values -> -19.247827 = (pi*(1-98.0664999999931/50))*50/(4*98.0664999999931/50).

FAQ

What is Eccentricity when Deflection in Eccentric Loading is Given?
The Outermost Fiber Distance when Deflection in Eccentric Loading is Given formula is defined as the distance in between the Neutral Axis and Outermost Fiber and is represented as e=(pi*(1-P/Pc))*𝜕 /(4*P/Pc) or Eccentricity of Loading=(pi*(1-Axial Load/Critical Buckling Load))*Deflection/(4*Axial Load/Critical Buckling Load). Axial Load is defined as applying a force on a structure directly along an axis of the structure, Critical Buckling Load is defined as the greatest load that will not cause lateral deflection and The Deflection is the degree to which a structural element is displaced under a load (due to its deformation). .
How to calculate Eccentricity when Deflection in Eccentric Loading is Given?
The Outermost Fiber Distance when Deflection in Eccentric Loading is Given formula is defined as the distance in between the Neutral Axis and Outermost Fiber is calculated using Eccentricity of Loading=(pi*(1-Axial Load/Critical Buckling Load))*Deflection/(4*Axial Load/Critical Buckling Load). To calculate Eccentricity when Deflection in Eccentric Loading is Given, you need Axial Load (P), Critical Buckling Load (Pc) and Deflection (𝜕 ). With our tool, you need to enter the respective value for Axial Load, Critical Buckling Load and Deflection 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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