Crippling Load on Column by Straight Line Formula given Slenderness Ratio Calculator

✖Compressive Stress is the internal resistance a material generates per unit area when subjected to a compressive force, which acts to reduce the volume or shorten the material.ⓘ Compressive Stress [σ_c]			+10% -10%
✖Straight Line Formula Constant is defined as the constant that depends on the material of column.ⓘ Straight Line Formula Constant [n]			+10% -10%
✖Slenderness Ratio is the ratio of the length of a column and the least radius of gyration of its cross section.ⓘ Slenderness Ratio [λ]			+10% -10%
✖Column Cross Sectional Area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specified axis at a point.ⓘ Column Cross Sectional Area [A_sectional]			+10% -10%

✖Crippling Load is the maximum load a structural member, such as a column or slender element, can carry before it experiences buckling or instability.ⓘ Crippling Load on Column by Straight Line Formula given Slenderness Ratio [P]

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Crippling Load on Column by Straight Line Formula given Slenderness Ratio Solution

STEP 0: Pre-Calculation Summary

Formula Used

Crippling Load = (Compressive Stress-(Straight Line Formula Constant*(Slenderness Ratio)))*Column Cross Sectional Area
P = (σ_c-(n*(λ)))*A_sectional
This formula uses 5 Variables

Variables Used

Crippling Load - (Measured in Newton) - Crippling Load is the maximum load a structural member, such as a column or slender element, can carry before it experiences buckling or instability.
Compressive Stress - (Measured in Pascal) - Compressive Stress is the internal resistance a material generates per unit area when subjected to a compressive force, which acts to reduce the volume or shorten the material.
Straight Line Formula Constant - Straight Line Formula Constant is defined as the constant that depends on the material of column.
Slenderness Ratio - Slenderness Ratio is the ratio of the length of a column and the least radius of gyration of its cross section.
Column Cross Sectional Area - (Measured in Square Meter) - Column Cross Sectional Area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specified axis at a point.

STEP 1: Convert Input(s) to Base Unit

Compressive Stress: 0.002827 Megapascal --> 2827 Pascal (Check conversion here)
Straight Line Formula Constant: 4 --> No Conversion Required
Slenderness Ratio: 0.5 --> No Conversion Required
Column Cross Sectional Area: 1.4 Square Meter --> 1.4 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

P = (σ_c-(n*(λ)))*A_sectional --> (2827-(4*(0.5)))*1.4

Evaluating ... ...

P = 3955

STEP 3: Convert Result to Output's Unit

3955 Newton -->3.955 Kilonewton (Check conversion here)

FINAL ANSWER

3.955 Kilonewton <-- Crippling Load

(Calculation completed in 00.004 seconds)

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< Straight Line Formula Calculators

Constant Depending on Material of Column by Straight-Line Formula for Columns and Struts

LaTeX Go Straight Line Formula Constant = (Compressive Stress-(Crippling Load/Column Cross Sectional Area))/((Effective Column Length/Least Radius of Gyration))

Cross-Sectional Area of Column by Straight-Line Formula for Columns and Struts

LaTeX Go Column Cross Sectional Area = Crippling Load/(Compressive Stress-(Straight Line Formula Constant*(Effective Column Length/Least Radius of Gyration)))

Compressive Yield Stress by Straight-Line Formula for Columns and Struts

LaTeX Go Compressive Stress = (Crippling Load/Column Cross Sectional Area)+(Straight Line Formula Constant*(Effective Column Length/Least Radius of Gyration))

Crippling Load on Column by Straight-Line Formula

LaTeX Go Crippling Load = (Compressive Stress-(Straight Line Formula Constant*(Effective Column Length/Least Radius of Gyration)))*Column Cross Sectional Area

Crippling Load on Column by Straight Line Formula given Slenderness Ratio Formula

LaTeX Go

Crippling Load = (Compressive Stress-(Straight Line Formula Constant*(Slenderness Ratio)))*Column Cross Sectional Area
P = (σ_c-(n*(λ)))*A_sectional

What is Crippling Load?

The Crippling Load, also known as the Critical Load or Buckling Load, refers to the maximum load a structural member, such as a column or slender element, can carry before it experiences buckling or instability.

How to Calculate Crippling Load on Column by Straight Line Formula given Slenderness Ratio?

Crippling Load on Column by Straight Line Formula given Slenderness Ratio calculator uses Crippling Load = (Compressive Stress-(Straight Line Formula Constant*(Slenderness Ratio)))*Column Cross Sectional Area to calculate the Crippling Load, Crippling Load on Column by Straight Line Formula given Slenderness Ratio formula is defined as the maximum load that a column can withstand before it gets deformed or buckled under compressive stress, taking into account the slenderness ratio of the column, which is a critical factor in determining its stability. Crippling Load is denoted by P symbol.

How to calculate Crippling Load on Column by Straight Line Formula given Slenderness Ratio using this online calculator? To use this online calculator for Crippling Load on Column by Straight Line Formula given Slenderness Ratio, enter Compressive Stress (σ_c), Straight Line Formula Constant (n), Slenderness Ratio (λ) & Column Cross Sectional Area (A_sectional) and hit the calculate button. Here is how the Crippling Load on Column by Straight Line Formula given Slenderness Ratio calculation can be explained with given input values -> 4.479997 = (2827-(4*(0.5)))*1.4.

FAQ

What is Crippling Load on Column by Straight Line Formula given Slenderness Ratio?

Crippling Load on Column by Straight Line Formula given Slenderness Ratio formula is defined as the maximum load that a column can withstand before it gets deformed or buckled under compressive stress, taking into account the slenderness ratio of the column, which is a critical factor in determining its stability and is represented as P = (σ_c-(n*(λ)))*A_sectional or Crippling Load = (Compressive Stress-(Straight Line Formula Constant*(Slenderness Ratio)))*Column Cross Sectional Area. Compressive Stress is the internal resistance a material generates per unit area when subjected to a compressive force, which acts to reduce the volume or shorten the material, Straight Line Formula Constant is defined as the constant that depends on the material of column, Slenderness Ratio is the ratio of the length of a column and the least radius of gyration of its cross section & Column Cross Sectional Area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specified axis at a point.

How to calculate Crippling Load on Column by Straight Line Formula given Slenderness Ratio?

Crippling Load on Column by Straight Line Formula given Slenderness Ratio formula is defined as the maximum load that a column can withstand before it gets deformed or buckled under compressive stress, taking into account the slenderness ratio of the column, which is a critical factor in determining its stability is calculated using Crippling Load = (Compressive Stress-(Straight Line Formula Constant*(Slenderness Ratio)))*Column Cross Sectional Area. To calculate Crippling Load on Column by Straight Line Formula given Slenderness Ratio, you need Compressive Stress (σ_c), Straight Line Formula Constant (n), Slenderness Ratio (λ) & Column Cross Sectional Area (A_sectional). With our tool, you need to enter the respective value for Compressive Stress, Straight Line Formula Constant, Slenderness Ratio & 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 Crippling Load?

In this formula, Crippling Load uses Compressive Stress, Straight Line Formula Constant, Slenderness Ratio & Column Cross Sectional Area. We can use 1 other way(s) to calculate the same, which is/are as follows -

Crippling Load = (Compressive Stress-(Straight Line Formula Constant*(Effective Column Length/Least Radius of Gyration)))*Column Cross Sectional Area

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