Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given 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%
✖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%
✖Total Unit Stress is defined as the the total force acting on unit area.ⓘ Total Unit Stress [f]			+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%

✖Moment of Inertia about Neutral Axis is defined as the moment of inertia of the beam about its neutral axisⓘ Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given [I]

⎘ Copy

👎 Report Issue!

👍 Share Now!

You are here:

Home »
Engineering »
Civil »
Beams »
Eccentric Loading »
Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given

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

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

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

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

Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given Formula

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

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

Total Unit Stress in Eccentric Loading when Radius of Gyration is Given GO

Eccentricity when Deflection in Eccentric Loading is Given GO

Define Moment of Inertia?

Moment of inertia, in physics, quantitative measure of the rotational inertia of a body—i.e., the opposition that the body exhibits to having its speed of rotation about an axis altered by the application of torque (turning force).

How to Calculate Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given?

Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given calculator uses Moment of Inertia about Neutral Axis=(Axial Load*Outermost Fiber Distance*Distance_from Load Applied)/(Total Unit Stress-(Axial Load/Cross sectional area)) to calculate the Moment of Inertia about Neutral Axis, The Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given formula is defined as the quantitative measure of the rotational inertia of a body. Moment of Inertia about Neutral Axis and is denoted by I symbol.

How to calculate Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given using this online calculator? To use this online calculator for Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given, enter Axial Load (P), Outermost Fiber Distance (c), Distance_from Load Applied (e), Total Unit Stress (f) and Cross sectional area (A) and hit the calculate button. Here is how the Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given calculation can be explained with given input values -> 0.001087 = (98.0664999999931*0.01*0.1)/(100-(98.0664999999931/10)).

FAQ

What is Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given?

The Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given formula is defined as the quantitative measure of the rotational inertia of a body and is represented as I=(P*c*e)/(f-(P/A)) or Moment of Inertia about Neutral Axis=(Axial Load*Outermost Fiber Distance*Distance_from Load Applied)/(Total Unit Stress-(Axial Load/Cross sectional area)). Axial Load is defined as applying a force on a structure directly along an axis of the structure, 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, Total Unit Stress is defined as the the total force acting on unit area and 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.

How to calculate Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given?

The Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given formula is defined as the quantitative measure of the rotational inertia of a body is calculated using Moment of Inertia about Neutral Axis=(Axial Load*Outermost Fiber Distance*Distance_from Load Applied)/(Total Unit Stress-(Axial Load/Cross sectional area)). To calculate Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given, you need Axial Load (P), Outermost Fiber Distance (c), Distance_from Load Applied (e), Total Unit Stress (f) and Cross sectional area (A). With our tool, you need to enter the respective value for Axial Load, Outermost Fiber Distance, Distance_from Load Applied, Total Unit Stress and Cross sectional area and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

Facebook
Twitter
WhatsApp
Reddit
LinkedIn
E-Mail

Let Others Know

✖

Facebook

Twitter

Copied!