Compressive Load given Stress Due to Direct Load for Long Column Calculator

✖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%
✖Direct Stress is defined as axial thrust acting per unit area.ⓘ Direct Stress [σ]			+10% -10%

✖Column Compressive load is the load applied to a column that is compressive in nature.ⓘ Compressive Load given Stress Due to Direct Load for Long Column [P_compressive]

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Formula

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Compressive Load given Stress Due to Direct Load for Long Column

Formula

`"P"_{"compressive"} = "A"_{"sectional"}*"σ"`

Example

`"0.375kN"="6.25m²"*"0.00006MPa"`

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Compressive Load given Stress Due to Direct Load for Long Column Solution

STEP 0: Pre-Calculation Summary

Formula Used

Column Compressive Load = Column Cross Sectional Area*Direct Stress
P_compressive = A_sectional*σ
This formula uses 3 Variables

Variables Used

Column Compressive Load - (Measured in Newton) - Column Compressive load is the load applied to a column that is compressive in nature.
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.
Direct Stress - (Measured in Pascal) - Direct Stress is defined as axial thrust acting per unit area.

STEP 1: Convert Input(s) to Base Unit

Column Cross Sectional Area: 6.25 Square Meter --> 6.25 Square Meter No Conversion Required
Direct Stress: 6E-05 Megapascal --> 60 Pascal (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

P_compressive = A_sectional*σ --> 6.25*60

Evaluating ... ...

P_compressive = 375

STEP 3: Convert Result to Output's Unit

375 Newton -->0.375 Kilonewton (Check conversion here)

FINAL ANSWER

0.375 Kilonewton <-- Column Compressive Load

(Calculation completed in 00.004 seconds)

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Created by Anshika Arya

National Institute Of Technology (NIT), Hamirpur

Anshika Arya has created this Calculator and 2000+ more calculators!

Verified by Payal Priya

Birsa Institute of Technology (BIT), Sindri

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< 15 Failure of a Column Calculators

Section Modulus about Axis of Bending for Long Column

Go Section Modulus = (Column Compressive Load*Column Maximum Bending)/Column Bending Stress

Area of Cross-Section given Compressive Stress Induced during Failure of Short Column

Go Column Cross Sectional Area = Column Compressive Load/Column Compressive Stress

Compressive Load given Compressive Stress Induced during Failure of Short Column

Go Column Compressive Load = Column Cross Sectional Area*Column Compressive Stress

Compressive Stress Induced during Failure of Short Column

Go Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area

Area of Cross-Section given Stress due to Direct Load for Long Column

Go Column Cross Sectional Area = Column Compressive Load/Direct Stress

Compressive Load given Stress Due to Direct Load for Long Column

Go Column Compressive Load = Column Cross Sectional Area*Direct Stress

Stress Due to Direct Load for Long Column

Go Direct Stress = Column Compressive Load/Column Cross Sectional Area

Area of Cross Section of Column given Crushing Stress

Go Column Cross Sectional Area = Crushing load/Column Crushing Stress

Crushing Stress for Short Column

Go Column Crushing Stress = Crushing load/Column Cross Sectional Area

Crushing Load for Short Column

Go Crushing load = Column Cross Sectional Area*Column Crushing Stress

Stress Due to Bending at Center of Column given Minimum Stress for Failure of Long Column

Go Column Bending Stress = Minimum Stress Value-Direct Stress

Minimum Stress for Failure of Long Column

Go Minimum Stress Value = Direct Stress+Column Bending Stress

Stress Due to Bending at Center of Column given Maximum Stress for Failure of Long Column

Go Column Bending Stress = Maximum Stress-Direct Stress

Stress Due to Direct Load given Maximum Stress for Failure of Long Column

Go Direct Stress = Maximum Stress-Column Bending Stress

Maximum Stress for Failure of Long Column

Go Maximum Stress = Direct Stress+Column Bending Stress

< 15 Modes of Failure in Eccentric Compression Calculators

Section Modulus about Axis of Bending for Long Column

Go Section Modulus = (Column Compressive Load*Column Maximum Bending)/Column Bending Stress

Area of Cross-Section given Compressive Stress Induced during Failure of Short Column

Go Column Cross Sectional Area = Column Compressive Load/Column Compressive Stress

Compressive Load given Compressive Stress Induced during Failure of Short Column

Go Column Compressive Load = Column Cross Sectional Area*Column Compressive Stress

Compressive Stress Induced during Failure of Short Column

Go Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area

Area of Cross-Section given Stress due to Direct Load for Long Column

Go Column Cross Sectional Area = Column Compressive Load/Direct Stress

Compressive Load given Stress Due to Direct Load for Long Column

Go Column Compressive Load = Column Cross Sectional Area*Direct Stress

Stress Due to Direct Load for Long Column

Go Direct Stress = Column Compressive Load/Column Cross Sectional Area

Area of Cross Section of Column given Crushing Stress

Go Column Cross Sectional Area = Crushing load/Column Crushing Stress

Crushing Stress for Short Column

Go Column Crushing Stress = Crushing load/Column Cross Sectional Area

Crushing Load for Short Column

Go Crushing load = Column Cross Sectional Area*Column Crushing Stress

Stress Due to Bending at Center of Column given Minimum Stress for Failure of Long Column

Go Column Bending Stress = Minimum Stress Value-Direct Stress

Minimum Stress for Failure of Long Column

Go Minimum Stress Value = Direct Stress+Column Bending Stress

Stress Due to Bending at Center of Column given Maximum Stress for Failure of Long Column

Go Column Bending Stress = Maximum Stress-Direct Stress

Stress Due to Direct Load given Maximum Stress for Failure of Long Column

Go Direct Stress = Maximum Stress-Column Bending Stress

Maximum Stress for Failure of Long Column

Go Maximum Stress = Direct Stress+Column Bending Stress

Compressive Load given Stress Due to Direct Load for Long Column Formula

Column Compressive Load = Column Cross Sectional Area*Direct Stress
P_compressive = A_sectional*σ

Where is Bending Stress Maximum?

The bottom die has a large deflection due to the bending force. The maximum bending stress occurs at the top surface of the die, and its location is corresponding to the inner bumps of the bottom die. The deflection of the beam is proportional to the bending moment, which is also proportional to the bending force.

How to Calculate Compressive Load given Stress Due to Direct Load for Long Column?

Compressive Load given Stress Due to Direct Load for Long Column calculator uses Column Compressive Load = Column Cross Sectional Area*Direct Stress to calculate the Column Compressive Load, The Compressive Load given Stress Due to Direct Load for Long Column formula is defined as the loads applied to a column are only axial loads. Loads on columns are typically applied at the ends of the member, producing axial compressive stresses. Column Compressive Load is denoted by P_compressive symbol.

How to calculate Compressive Load given Stress Due to Direct Load for Long Column using this online calculator? To use this online calculator for Compressive Load given Stress Due to Direct Load for Long Column, enter Column Cross Sectional Area (A_sectional) & Direct Stress (σ) and hit the calculate button. Here is how the Compressive Load given Stress Due to Direct Load for Long Column calculation can be explained with given input values -> 0.000375 = 6.25*60.

FAQ

What is Compressive Load given Stress Due to Direct Load for Long Column?

The Compressive Load given Stress Due to Direct Load for Long Column formula is defined as the loads applied to a column are only axial loads. Loads on columns are typically applied at the ends of the member, producing axial compressive stresses and is represented as P_compressive = A_sectional*σ or Column Compressive Load = Column Cross Sectional Area*Direct Stress. 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 & Direct Stress is defined as axial thrust acting per unit area.

How to calculate Compressive Load given Stress Due to Direct Load for Long Column?

The Compressive Load given Stress Due to Direct Load for Long Column formula is defined as the loads applied to a column are only axial loads. Loads on columns are typically applied at the ends of the member, producing axial compressive stresses is calculated using Column Compressive Load = Column Cross Sectional Area*Direct Stress. To calculate Compressive Load given Stress Due to Direct Load for Long Column, you need Column Cross Sectional Area (A_sectional) & Direct Stress (σ). With our tool, you need to enter the respective value for Column Cross Sectional Area & Direct Stress 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 Column Compressive Load?

In this formula, Column Compressive Load uses Column Cross Sectional Area & Direct Stress. We can use 2 other way(s) to calculate the same, which is/are as follows -

Column Compressive Load = Column Cross Sectional Area*Column Compressive Stress
Column Compressive Load = Column Cross Sectional Area*Column Compressive Stress

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