Maximum Load on Axially Loaded Members Formula

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Maximum Axial Load is the load acting through the longitudinal axis of the section. Check FAQs
Pu=0.85AgFcr
Pu - Maximum Axial Load?Ag - Gross Cross-Sectional Area?Fcr - Critical Buckling Stress?

Maximum Load on Axially Loaded Members Example

With values
With units
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Here is how the Maximum Load on Axially Loaded Members equation looks like with Values.

Here is how the Maximum Load on Axially Loaded Members equation looks like with Units.

Here is how the Maximum Load on Axially Loaded Members equation looks like.

296.82Edit=0.853600Edit97Edit
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Maximum Load on Axially Loaded Members Solution

Follow our step by step solution on how to calculate Maximum Load on Axially Loaded Members?

FIRST Step Consider the formula
Pu=0.85AgFcr
Next Step Substitute values of Variables
Pu=0.853600mm²97MPa
Next Step Convert Units
Pu=0.850.00369.7E+7Pa
Next Step Prepare to Evaluate
Pu=0.850.00369.7E+7
Next Step Evaluate
Pu=296820N
LAST Step Convert to Output's Unit
Pu=296.82kN

Maximum Load on Axially Loaded Members Formula Elements

Variables
Maximum Axial Load
Maximum Axial Load is the load acting through the longitudinal axis of the section.
Symbol: Pu
Measurement: ForceUnit: kN
Note: Value should be greater than 0.
Gross Cross-Sectional Area
Gross Cross-Sectional Area is the total area of the cross-section of a structural member, such as a beam or column, measured in a plane perpendicular to the member's longitudinal axis.
Symbol: Ag
Measurement: AreaUnit: mm²
Note: Value should be greater than 0.
Critical Buckling Stress
Critical Buckling Stress is the maximum stress that can be taken by the section without failure. Any stress surpassing the critical stress makes the section, say, column to failure.
Symbol: Fcr
Measurement: StressUnit: MPa
Note: Value should be greater than 0.

Other formulas in Columns category

​Go Critical Buckling Stress when Slenderness Parameter is Less than 2.25
Fcr=0.658λcFy
​Go Critical Buckling Stress when Slenderness Parameter is greater than 2.25
Fcr=0.877Fyλc
​Go Slenderness Parameter
λc=(klr)2(Fy286220)

How to Evaluate Maximum Load on Axially Loaded Members?

Maximum Load on Axially Loaded Members evaluator uses Maximum Axial Load = 0.85*Gross Cross-Sectional Area*Critical Buckling Stress to evaluate the Maximum Axial Load, The Maximum Load on Axially Loaded Members formula is defined as the greatest amount of axial force that a structural member (such as a column or strut) can safely carry without experiencing failure. The maximum load is determined based on the member's material properties, cross-sectional area, length, and boundary conditions, ensuring that the member does not exceed its yield strength or buckling capacity. Maximum Axial Load is denoted by Pu symbol.

How to evaluate Maximum Load on Axially Loaded Members using this online evaluator? To use this online evaluator for Maximum Load on Axially Loaded Members, enter Gross Cross-Sectional Area (Ag) & Critical Buckling Stress (Fcr) and hit the calculate button.

FAQs on Maximum Load on Axially Loaded Members

What is the formula to find Maximum Load on Axially Loaded Members?
The formula of Maximum Load on Axially Loaded Members is expressed as Maximum Axial Load = 0.85*Gross Cross-Sectional Area*Critical Buckling Stress. Here is an example- 0.29682 = 0.85*0.0036*97000000.
How to calculate Maximum Load on Axially Loaded Members?
With Gross Cross-Sectional Area (Ag) & Critical Buckling Stress (Fcr) we can find Maximum Load on Axially Loaded Members using the formula - Maximum Axial Load = 0.85*Gross Cross-Sectional Area*Critical Buckling Stress.
Can the Maximum Load on Axially Loaded Members be negative?
No, the Maximum Load on Axially Loaded Members, measured in Force cannot be negative.
Which unit is used to measure Maximum Load on Axially Loaded Members?
Maximum Load on Axially Loaded Members is usually measured using the Kilonewton[kN] for Force. Newton[kN], Exanewton[kN], Meganewton[kN] are the few other units in which Maximum Load on Axially Loaded Members can be measured.
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