Total Unit Stress in Eccentric Loading when Radius of Gyration 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%
✖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%
✖Radius of gyration or gyradius of a body about an axis of rotation is defined as the radial distance to a point which would have a moment of inertia the same as the body's actual distribution of mass, if the total mass of the body were concentrated there.ⓘ Radius of gyration [k_G]			+10% -10%

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

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

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

Periodic time of SHM for compound pendulum in terms of radius of gyration

Periodic time for compound pendulum=2*pi*sqrt(((Radius of gyration^2)+(Distance of point of suspension of pendulum from the center of gravity^2))/(Acceleration Due To Gravity*Distance of point of suspension of pendulum from the center of gravity)) GO

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

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

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

Time period of Rolling

Time period of rolling=2*pi*(sqrt(((Radius of gyration)^(2))/(Acceleration Due To Gravity*Metacentric height))) GO

Minimum periodic time of SHM for compound pendulum

Time Period SHM=2*pi*sqrt(2*Radius of gyration/Acceleration Due To Gravity) 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

Total Unit Stress=(Axial Load/Cross sectional area)+(Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis) GO

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

Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2)))
f=(P/A)*(1+(c*e/(k<sub>G</sub>^2)))

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

Eccentricity when Deflection in Eccentric Loading is Given GO

Define Radius of Gyration?

The radius of gyration or gyradius of a body about an axis of rotation is defined as the radial distance to a point that would have a moment of inertia the same as the body's actual distribution of mass if the total mass of the body were concentrated there

How to Calculate Total Unit Stress in Eccentric Loading when Radius of Gyration is Given?

Total Unit Stress in Eccentric Loading when Radius of Gyration is Given calculator uses Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2))) to calculate the Total Unit Stress, The Total Unit Stress in Eccentric Loading when Radius of Gyration is Given formula is defined as the total force applied on a body acting on a unit area. Total Unit Stress and is denoted by f symbol.

How to calculate Total Unit Stress in Eccentric Loading when Radius of Gyration is Given using this online calculator? To use this online calculator for Total Unit Stress in Eccentric Loading when Radius of Gyration is Given, enter Axial Load (P), Cross sectional area (A), Outermost Fiber Distance (c), Distance_from Load Applied (e) and Radius of gyration (k_G) and hit the calculate button. Here is how the Total Unit Stress in Eccentric Loading when Radius of Gyration is Given calculation can be explained with given input values -> 9.80774 = (98.0664999999931/10)*(1+(0.01*0.1/(3^2))).

FAQ

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

The Total Unit Stress in Eccentric Loading when Radius of Gyration is Given formula is defined as the total force applied on a body acting on a unit area and is represented as f=(P/A)*(1+(c*e/(k_G^2))) or Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2))). 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 Radius of gyration or gyradius of a body about an axis of rotation is defined as the radial distance to a point which would have a moment of inertia the same as the body's actual distribution of mass, if the total mass of the body were concentrated there.

How to calculate Total Unit Stress in Eccentric Loading when Radius of Gyration is Given?

The Total Unit Stress in Eccentric Loading when Radius of Gyration is Given formula is defined as the total force applied on a body acting on a unit area is calculated using Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2))). To calculate Total Unit Stress in Eccentric Loading when Radius of Gyration is Given, you need Axial Load (P), Cross sectional area (A), Outermost Fiber Distance (c), Distance_from Load Applied (e) and Radius of gyration (k_G). With our tool, you need to enter the respective value for Axial Load, Cross sectional area, Outermost Fiber Distance, Distance_from Load Applied and Radius of gyration 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 Radius of gyration. We can use 1 other way(s) to calculate the same, which is/are as follows -

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

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