Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load Solution

STEP 0: Pre-Calculation Summary
Formula Used
Axial Thrust = (Maximum Bending Stress-(Maximum Bending Moment In Column/Modulus of Elasticity of Column))*Cross Sectional Area
Paxial = (σbmax-(M/εcolumn))*Asectional
This formula uses 5 Variables
Variables Used
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.
Maximum Bending Stress - (Measured in Pascal) - Maximum Bending Stress is the highest stress experienced by a material subjected to a bending load.
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.
Modulus of Elasticity of Column - (Measured in Pascal) - Modulus of Elasticity of Column is a quantity that measures column's resistance to being deformed elastically when stress is applied to it.
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.
STEP 1: Convert Input(s) to Base Unit
Maximum Bending Stress: 2 Megapascal --> 2000000 Pascal (Check conversion ​here)
Maximum Bending Moment In Column: 16 Newton Meter --> 16 Newton Meter No Conversion Required
Modulus of Elasticity of Column: 10.56 Megapascal --> 10560000 Pascal (Check conversion ​here)
Cross Sectional Area: 1.4 Square Meter --> 1.4 Square Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Paxial = (σbmax-(M/εcolumn))*Asectional --> (2000000-(16/10560000))*1.4
Evaluating ... ...
Paxial = 2799999.99999788
STEP 3: Convert Result to Output's Unit
2799999.99999788 Newton --> No Conversion Required
FINAL ANSWER
2799999.99999788 2.8E+6 Newton <-- Axial Thrust
(Calculation completed in 00.020 seconds)

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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))

Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load Formula

​LaTeX ​Go
Axial Thrust = (Maximum Bending Stress-(Maximum Bending Moment In Column/Modulus of Elasticity of Column))*Cross Sectional Area
Paxial = (σbmax-(M/εcolumn))*Asectional

What is Axial Thrust?

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

How to Calculate Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load?

Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load calculator uses Axial Thrust = (Maximum Bending Stress-(Maximum Bending Moment In Column/Modulus of Elasticity of Column))*Cross Sectional Area to calculate the Axial Thrust, The Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load formula is defined as a measure of the compressive force exerted on a strut when it is subjected to both axial thrust and a transverse uniformly distributed load, taking into account the elastic modulus of the material and the sectional area of the strut. Axial Thrust is denoted by Paxial symbol.

How to calculate Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load using this online calculator? To use this online calculator for Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load, enter Maximum Bending Stress (σbmax), Maximum Bending Moment In Column (M), Modulus of Elasticity of Column column) & Cross Sectional Area (Asectional) and hit the calculate button. Here is how the Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load calculation can be explained with given input values -> 2.8E+6 = (2000000-(16/10560000))*1.4.

FAQ

What is Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load?
The Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load formula is defined as a measure of the compressive force exerted on a strut when it is subjected to both axial thrust and a transverse uniformly distributed load, taking into account the elastic modulus of the material and the sectional area of the strut and is represented as Paxial = (σbmax-(M/εcolumn))*Asectional or Axial Thrust = (Maximum Bending Stress-(Maximum Bending Moment In Column/Modulus of Elasticity of Column))*Cross Sectional Area. Maximum Bending Stress is the highest stress experienced by a material subjected to a bending load, Maximum Bending Moment In Column is the highest amount of bending force that a column experiences due to applied loads, either axial or eccentric, Modulus of Elasticity of Column is a quantity that measures column's resistance to being deformed elastically when stress is applied to it & 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.
How to calculate Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load?
The Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load formula is defined as a measure of the compressive force exerted on a strut when it is subjected to both axial thrust and a transverse uniformly distributed load, taking into account the elastic modulus of the material and the sectional area of the strut is calculated using Axial Thrust = (Maximum Bending Stress-(Maximum Bending Moment In Column/Modulus of Elasticity of Column))*Cross Sectional Area. To calculate Axial Thrust given Elastic Modulus for Strut subjected to Uniformly Distributed Load, you need Maximum Bending Stress (σbmax), Maximum Bending Moment In Column (M), Modulus of Elasticity of Column column) & Cross Sectional Area (Asectional). With our tool, you need to enter the respective value for Maximum Bending Stress, Maximum Bending Moment In Column, Modulus of Elasticity of Column & Cross Sectional Area 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 Axial Thrust?
In this formula, Axial Thrust uses Maximum Bending Stress, Maximum Bending Moment In Column, Modulus of Elasticity of Column & Cross Sectional Area. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • 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
  • Axial Thrust = (-Maximum Bending Moment In Column-(Load Intensity*(Column Length^2)/8))/(Maximum Initial Deflection)
  • Axial Thrust = (Maximum Bending Stress-(Maximum Bending Moment In Column*Distance from Neutral Axis to Extreme Point/Moment of Inertia))*Cross Sectional Area
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