Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut Solution

STEP 0: Pre-Calculation Summary
Formula Used
Distance from Neutral Axis to Extreme Point = Bending Stress in Column*(Column Cross Sectional Area*(Least Radius of Gyration of Column^2))/(Bending Moment in Column)
c = σb*(Asectional*(k^2))/(Mb)
This formula uses 5 Variables
Variables Used
Distance from Neutral Axis to Extreme Point - (Measured in Meter) - Distance from Neutral Axis to Extreme Point is the distance between the neutral axis and the extreme point.
Bending Stress in Column - (Measured in Pascal) - Bending Stress in Column is the normal stress that is induced at a point in a column subjected to loads that cause it to bend.
Column Cross Sectional Area - (Measured in Square Meter) - Column Cross Sectional Area is the area of a column that is obtained when a column is sliced perpendicular to some specified axis at a point.
Least Radius of Gyration of Column - (Measured in Meter) - Least Radius of Gyration of Column is a measure of the distribution of its cross-sectional area around its centroidal axis.
Bending Moment in Column - (Measured in Newton Meter) - Bending Moment in Column is the reaction induced in a column when an external force or moment is applied to the element, causing the element to bend.
STEP 1: Convert Input(s) to Base Unit
Bending Stress in Column: 0.04 Megapascal --> 40000 Pascal (Check conversion ​here)
Column Cross Sectional Area: 1.4 Square Meter --> 1.4 Square Meter No Conversion Required
Least Radius of Gyration of Column: 2.9277 Millimeter --> 0.0029277 Meter (Check conversion ​here)
Bending Moment in Column: 48 Newton Meter --> 48 Newton Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
c = σb*(Asectional*(k^2))/(Mb) --> 40000*(1.4*(0.0029277^2))/(48)
Evaluating ... ...
c = 0.009999998505
STEP 3: Convert Result to Output's Unit
0.009999998505 Meter -->9.999998505 Millimeter (Check conversion ​here)
FINAL ANSWER
9.999998505 9.999999 Millimeter <-- Distance from Neutral Axis to Extreme Point
(Calculation completed in 00.004 seconds)

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Strut Subjected to Compressive Axial Thrust and a Transverse Point Load at the Centre Calculators

Deflection at Section for Strut with Axial and Transverse Point Load at Center
​ LaTeX ​ Go Deflection at Column Section = Column Compressive Load-(Bending Moment in Column+(Greatest Safe Load*Distance of Deflection from end A/2))/(Column Compressive Load)
Compressive Axial Load for Strut with Axial and Transverse Point Load at Center
​ LaTeX ​ Go Column Compressive Load = -(Bending Moment in Column+(Greatest Safe Load*Distance of Deflection from end A/2))/(Deflection at Column Section)
Transverse Point Load for Strut with Axial and Transverse Point Load at Center
​ LaTeX ​ Go Greatest Safe Load = (-Bending Moment in Column-(Column Compressive Load*Deflection at Column Section))*2/(Distance of Deflection from end A)
Bending Moment at Section for Strut with Axial and Transverse Point Load at Center
​ LaTeX ​ Go Bending Moment in Column = -(Column Compressive Load*Deflection at Column Section)-(Greatest Safe Load*Distance of Deflection from end A/2)

Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut Formula

​LaTeX ​Go
Distance from Neutral Axis to Extreme Point = Bending Stress in Column*(Column Cross Sectional Area*(Least Radius of Gyration of Column^2))/(Bending Moment in Column)
c = σb*(Asectional*(k^2))/(Mb)

What is transverse point loading?

Transverse loading is a load applied vertically to the plane of the longitudinal axis of a configuration, such as a wind load. It causes the material to bend and rebound from its original position, with inner tensile and compressive straining associated with the change in curvature of the material.

How to Calculate Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut?

Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut calculator uses Distance from Neutral Axis to Extreme Point = Bending Stress in Column*(Column Cross Sectional Area*(Least Radius of Gyration of Column^2))/(Bending Moment in Column) to calculate the Distance from Neutral Axis to Extreme Point, The Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut formula is defined as the measure of the distance from the neutral axis to the extreme layer of a strut subjected to compressive axial thrust and a transverse point load at the center, providing insight into the structural integrity of the strut under various loads. Distance from Neutral Axis to Extreme Point is denoted by c symbol.

How to calculate Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut using this online calculator? To use this online calculator for Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut, enter Bending Stress in Column b), Column Cross Sectional Area (Asectional), Least Radius of Gyration of Column (k) & Bending Moment in Column (Mb) and hit the calculate button. Here is how the Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut calculation can be explained with given input values -> 2.6E+6 = 40000*(1.4*(0.0029277^2))/(48).

FAQ

What is Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut?
The Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut formula is defined as the measure of the distance from the neutral axis to the extreme layer of a strut subjected to compressive axial thrust and a transverse point load at the center, providing insight into the structural integrity of the strut under various loads and is represented as c = σb*(Asectional*(k^2))/(Mb) or Distance from Neutral Axis to Extreme Point = Bending Stress in Column*(Column Cross Sectional Area*(Least Radius of Gyration of Column^2))/(Bending Moment in Column). Bending Stress in Column is the normal stress that is induced at a point in a column subjected to loads that cause it to bend, Column Cross Sectional Area is the area of a column that is obtained when a column is sliced perpendicular to some specified axis at a point, Least Radius of Gyration of Column is a measure of the distribution of its cross-sectional area around its centroidal axis & Bending Moment in Column is the reaction induced in a column when an external force or moment is applied to the element, causing the element to bend.
How to calculate Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut?
The Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut formula is defined as the measure of the distance from the neutral axis to the extreme layer of a strut subjected to compressive axial thrust and a transverse point load at the center, providing insight into the structural integrity of the strut under various loads is calculated using Distance from Neutral Axis to Extreme Point = Bending Stress in Column*(Column Cross Sectional Area*(Least Radius of Gyration of Column^2))/(Bending Moment in Column). To calculate Distance of Extreme Layer from Neutral Axis given Bending Stress for Strut, you need Bending Stress in Column b), Column Cross Sectional Area (Asectional), Least Radius of Gyration of Column (k) & Bending Moment in Column (Mb). With our tool, you need to enter the respective value for Bending Stress in Column, Column Cross Sectional Area, Least Radius of Gyration of Column & Bending Moment in Column 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 Distance from Neutral Axis to Extreme Point?
In this formula, Distance from Neutral Axis to Extreme Point uses Bending Stress in Column, Column Cross Sectional Area, Least Radius of Gyration of Column & Bending Moment in Column. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Distance from Neutral Axis to Extreme Point = Maximum Bending Stress*(Column Cross Sectional Area*(Least Radius of Gyration of Column^2))/(Maximum Bending Moment In Column)
  • Distance from Neutral Axis to Extreme Point = (Maximum Bending Stress-(Column Compressive Load/Column Cross Sectional Area))*(Column Cross Sectional Area*(Least Radius of Gyration of Column^2))/((Greatest Safe Load*(((sqrt(Moment of Inertia in Column*Modulus of Elasticity/Column Compressive Load))/(2*Column Compressive Load))*tan((Column Length/2)*(sqrt(Column Compressive Load/(Moment of Inertia in Column*Modulus of Elasticity/Column Compressive Load)))))))
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