Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load Calculator

✖Maximum Bending Stress is the highest stress experienced by a material subjected to a bending load.ⓘ Maximum Bending Stress [σb^max]			+10% -10%
✖Axial Thrust is the force exerted along the axis of a shaft in mechanical systems. It occurs when there is an imbalance of forces that acts in the direction parallel to the axis of rotation.ⓘ Axial Thrust [P_axial]			+10% -10%
✖Cross Sectional Area of Column is the area of a column that is obtained when a column is sliced perpendicular to some specified axis at a point.ⓘ Cross Sectional Area [A_sectional]			+10% -10%
✖Moment of Inertia is the measure of the resistance of a body to angular acceleration about a given axis.ⓘ Moment of Inertia [I]			+10% -10%
✖Maximum Bending Moment In Column is the highest amount of bending force that a column experiences due to applied loads, either axial or eccentric.ⓘ Maximum Bending Moment In Column [M]			+10% -10%

✖Distance from Neutral Axis to Extreme Point is the distance between the neutral axis and the extreme point.ⓘ Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load [c]

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Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load Solution

STEP 0: Pre-Calculation Summary

Formula Used

Distance from Neutral Axis to Extreme Point = (Maximum Bending Stress-(Axial Thrust/Cross Sectional Area))*Moment of Inertia/(Maximum Bending Moment In Column)
c = (σb^max-(P_axial/A_sectional))*I/(M)
This formula uses 6 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.
Maximum Bending Stress - (Measured in Pascal) - Maximum Bending Stress is the highest stress experienced by a material subjected to a bending load.
Axial Thrust - (Measured in Newton) - Axial Thrust is the force exerted along the axis of a shaft in mechanical systems. It occurs when there is an imbalance of forces that acts in the direction parallel to the axis of rotation.
Cross Sectional Area - (Measured in Square Meter) - Cross Sectional Area of Column is the area of a column that is obtained when a column is sliced perpendicular to some specified axis at a point.
Moment of Inertia - (Measured in Meter⁴) - Moment of Inertia is the measure of the resistance of a body to angular acceleration about a given axis.
Maximum Bending Moment In Column - (Measured in Newton Meter) - Maximum Bending Moment In Column is the highest amount of bending force that a column experiences due to applied loads, either axial or eccentric.

STEP 1: Convert Input(s) to Base Unit

Maximum Bending Stress: 2 Megapascal --> 2000000 Pascal (Check conversion here)
Axial Thrust: 1500 Newton --> 1500 Newton No Conversion Required
Cross Sectional Area: 1.4 Square Meter --> 1.4 Square Meter No Conversion Required
Moment of Inertia: 5600 Centimeter⁴ --> 5.6E-05 Meter⁴ (Check conversion here)
Maximum Bending Moment In Column: 16 Newton Meter --> 16 Newton Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

c = (σb^max-(P_axial/A_sectional))*I/(M) --> (2000000-(1500/1.4))*5.6E-05/(16)

Evaluating ... ...

c = 6.99625

STEP 3: Convert Result to Output's Unit

6.99625 Meter -->6996.25 Millimeter (Check conversion here)

FINAL ANSWER

6996.25 Millimeter <-- Distance from Neutral Axis to Extreme Point

(Calculation completed in 00.004 seconds)

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Home » Physics » Strength of Materials » Column And Struts » Strut With Lateral Load » Mechanical » Strut Subjected to Compressive Axial Thrust and a Transverse Uniformly Distributed Load » Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load

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< Strut Subjected to Compressive Axial Thrust and a Transverse Uniformly Distributed Load Calculators

Bending Moment at Section for Strut subjected to Compressive Axial and Uniformly Distributed Load

LaTeX Go Bending Moment in Column = -(Axial Thrust*Deflection at Section of Column)+(Load Intensity*(((Distance of Deflection from End A^2)/2)-(Column Length*Distance of Deflection from End A/2)))

Deflection at Section for Strut Subjected to Compressive Axial and Uniformly Distributed Load

LaTeX Go Deflection at Section of Column = (-Bending Moment in Column+(Load Intensity*(((Distance of Deflection from End A^2)/2)-(Column Length*Distance of Deflection from End A/2))))/Axial Thrust

Axial Thrust for Strut Subjected to Compressive Axial and Uniformly Distributed Load

LaTeX Go Axial Thrust = (-Bending Moment in Column+(Load Intensity*(((Distance of Deflection from End A^2)/2)-(Column Length*Distance of Deflection from End A/2))))/Deflection at Section of Column

Load Intensity for Strut Subjected to Compressive Axial and Uniformly Distributed Load

LaTeX Go Load Intensity = (Bending Moment in Column+(Axial Thrust*Deflection at Section of Column))/(((Distance of Deflection from End A^2)/2)-(Column Length*Distance of Deflection from End A/2))

Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load Formula

LaTeX Go

What is Axial Thrust?

Axial thrust refers to a propelling force applied along the axis (also called axial direction) of an object to push the object against a platform in a particular direction.

How to Calculate Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load?

Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load calculator uses Distance from Neutral Axis to Extreme Point = (Maximum Bending Stress-(Axial Thrust/Cross Sectional Area))*Moment of Inertia/(Maximum Bending Moment In Column) to calculate the Distance from Neutral Axis to Extreme Point, The Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load formula is defined as a measure of the maximum stress a strut can withstand under compressive axial thrust and transverse uniformly distributed load, providing critical information for structural integrity and safety assessments. Distance from Neutral Axis to Extreme Point is denoted by c symbol.

How to calculate Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load using this online calculator? To use this online calculator for Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load, enter Maximum Bending Stress (σb^max), Axial Thrust (P_axial), Cross Sectional Area (A_sectional), Moment of Inertia (I) & Maximum Bending Moment In Column (M) and hit the calculate button. Here is how the Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load calculation can be explained with given input values -> 7E+6 = (2000000-(1500/1.4))*5.6E-05/(16).

FAQ

What is Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load?

The Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load formula is defined as a measure of the maximum stress a strut can withstand under compressive axial thrust and transverse uniformly distributed load, providing critical information for structural integrity and safety assessments and is represented as c = (σb^max-(P_axial/A_sectional))*I/(M) or Distance from Neutral Axis to Extreme Point = (Maximum Bending Stress-(Axial Thrust/Cross Sectional Area))*Moment of Inertia/(Maximum Bending Moment In Column). Maximum Bending Stress is the highest stress experienced by a material subjected to a bending load, Axial Thrust is the force exerted along the axis of a shaft in mechanical systems. It occurs when there is an imbalance of forces that acts in the direction parallel to the axis of rotation, Cross Sectional Area of Column is the area of a column that is obtained when a column is sliced perpendicular to some specified axis at a point, Moment of Inertia is the measure of the resistance of a body to angular acceleration about a given axis & Maximum Bending Moment In Column is the highest amount of bending force that a column experiences due to applied loads, either axial or eccentric.

How to calculate Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load?

The Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load formula is defined as a measure of the maximum stress a strut can withstand under compressive axial thrust and transverse uniformly distributed load, providing critical information for structural integrity and safety assessments is calculated using Distance from Neutral Axis to Extreme Point = (Maximum Bending Stress-(Axial Thrust/Cross Sectional Area))*Moment of Inertia/(Maximum Bending Moment In Column). To calculate Distance of Extreme Layer from NA given Max Stress for Strut under Uniformly Distributed Load, you need Maximum Bending Stress (σb^max), Axial Thrust (P_axial), Cross Sectional Area (A_sectional), Moment of Inertia (I) & Maximum Bending Moment In Column (M). With our tool, you need to enter the respective value for Maximum Bending Stress, Axial Thrust, Cross Sectional Area, Moment of Inertia & Maximum 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.

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