Compressive Stress Induced during Failure of Short Column Calculator

✖Column Compressive load is the load applied to a column that is compressive in nature.ⓘ Column Compressive Load [P_compressive]			+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%

✖Column Compressive Stress is the force that is responsible for the deformation of the material such that the volume of the material reduces.ⓘ Compressive Stress Induced during Failure of Short Column [σ_c]

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Formula

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Compressive Stress Induced during Failure of Short Column

Formula

`"σ"_{"c"} = "P"_{"compressive"}/"A"_{"sectional"}`

Example

`"6.4E^-5MPa"="0.4kN"/"6.25m²"`

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Compressive Stress Induced during Failure of Short Column Solution

STEP 0: Pre-Calculation Summary

Formula Used

Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area
σ_c = P_compressive/A_sectional
This formula uses 3 Variables

Variables Used

Column Compressive Stress - (Measured in Pascal) - Column Compressive Stress is the force that is responsible for the deformation of the material such that the volume of the material reduces.
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.

STEP 1: Convert Input(s) to Base Unit

Column Compressive Load: 0.4 Kilonewton --> 400 Newton (Check conversion here)
Column Cross Sectional Area: 6.25 Square Meter --> 6.25 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

σ_c = P_compressive/A_sectional --> 400/6.25

Evaluating ... ...

σ_c = 64

STEP 3: Convert Result to Output's Unit

64 Pascal -->6.4E-05 Megapascal (Check conversion here)

FINAL ANSWER

6.4E-05 ≈ 6.4E-5 Megapascal <-- Column Compressive Stress

(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 Stress Induced during Failure of Short Column Formula

Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area
σ_c = P_compressive/A_sectional

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 Stress Induced during Failure of Short Column?

Compressive Stress Induced during Failure of Short Column calculator uses Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area to calculate the Column Compressive Stress, The Compressive Stress Induced during Failure of Short Column formula is defined as the force that is responsible for the deformation of the material such that the volume of the material reduces. Column Compressive Stress is denoted by σ_c symbol.

How to calculate Compressive Stress Induced during Failure of Short Column using this online calculator? To use this online calculator for Compressive Stress Induced during Failure of Short Column, enter Column Compressive Load (P_compressive) & Column Cross Sectional Area (A_sectional) and hit the calculate button. Here is how the Compressive Stress Induced during Failure of Short Column calculation can be explained with given input values -> 6.4E-11 = 400/6.25.

FAQ

What is Compressive Stress Induced during Failure of Short Column?

The Compressive Stress Induced during Failure of Short Column formula is defined as the force that is responsible for the deformation of the material such that the volume of the material reduces and is represented as σ_c = P_compressive/A_sectional or Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area. Column Compressive load is the load applied to a column that is compressive in nature & 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 Compressive Stress Induced during Failure of Short Column?

The Compressive Stress Induced during Failure of Short Column formula is defined as the force that is responsible for the deformation of the material such that the volume of the material reduces is calculated using Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area. To calculate Compressive Stress Induced during Failure of Short Column, you need Column Compressive Load (P_compressive) & Column Cross Sectional Area (A_sectional). With our tool, you need to enter the respective value for Column Compressive Load & 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.

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