Ultimate Crushing Stress given Crushing Load Solution

STEP 0: Pre-Calculation Summary
Formula Used
Column Crushing Stress = Crushing Load/Column Cross Sectional Area
σc = Pc/A
This formula uses 3 Variables
Variables Used
Column Crushing Stress - (Measured in Pascal) - Column Crushing stress is a special type of localized compressive stress which occurs at the surface of contact of two members that are relatively at rest.
Crushing Load - (Measured in Newton) - Crushing Load is the intensity of load required to crush the material.
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
Crushing Load: 1500 Kilonewton --> 1500000 Newton (Check conversion ​here)
Column Cross Sectional Area: 2000 Square Millimeter --> 0.002 Square Meter (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σc = Pc/A --> 1500000/0.002
Evaluating ... ...
σc = 750000000
STEP 3: Convert Result to Output's Unit
750000000 Pascal -->750 Megapascal (Check conversion ​here)
FINAL ANSWER
750 Megapascal <-- Column Crushing Stress
(Calculation completed in 00.004 seconds)

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19 Euler and Rankine's Theory Calculators

Effective Length of Column given Crippling Load and Rankine's Constant
​ Go Effective Column Length = sqrt((Column Crushing Stress*Column Cross Sectional Area/Crippling Load-1)*(Least Radius of Gyration Column^2)/Rankine's Constant)
Least Radius of Gyration given Crippling Load and Rankine's Constant
​ Go Least Radius of Gyration Column = sqrt((Rankine's Constant*Effective Column Length^2)/(Column Crushing Stress*Column Cross Sectional Area/Crippling Load-1))
Rankine's Constant given Crippling Load
​ Go Rankine's Constant = ((Column Crushing Stress*Column Cross Sectional Area)/Crippling Load-1)*((Least Radius of Gyration Column)/Effective Column Length)^2
Cross-Sectional Area of Column given Crippling Load and Rankine's Constant
​ Go Column Cross Sectional Area = (Crippling Load*(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2))/Column Crushing Stress
Ultimate Crushing Stress given Crippling Load and Rankine's Constant
​ Go Column Crushing Stress = (Crippling Load*(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2))/Column Cross Sectional Area
Crippling Load given Rankine's Constant
​ Go Crippling Load = (Column Crushing Stress*Column Cross Sectional Area)/(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2)
Effective Length of Column given Crippling Load by Euler's Formula
​ Go Effective Column Length = sqrt((pi^2*Modulus of Elasticity Column*Moment of Inertia Column)/(Euler’s Buckling Load))
Crushing Load by Rankine's Formula
​ Go Crushing Load = (Rankine’s Critical Load*Euler’s Buckling Load)/(Euler’s Buckling Load-Rankine’s Critical Load)
Crippling Load by Euler's Formula given Crippling Load by Rankine's Formula
​ Go Euler’s Buckling Load = (Crushing Load*Rankine’s Critical Load)/(Crushing Load-Rankine’s Critical Load)
Crippling Load by Rankine's Formula
​ Go Rankine’s Critical Load = (Crushing Load*Euler’s Buckling Load)/(Crushing Load+Euler’s Buckling Load)
Modulus of Elasticity given Crippling Load by Euler's Formula
​ Go Modulus of Elasticity Column = (Euler’s Buckling Load*Effective Column Length^2)/(pi^2*Moment of Inertia Column)
Moment of Inertia given Crippling Load by Euler's Formula
​ Go Moment of Inertia Column = (Euler’s Buckling Load*Effective Column Length^2)/(pi^2*Modulus of Elasticity Column)
Crippling Load by Euler's Formula
​ Go Euler’s Buckling Load = (pi^2*Modulus of Elasticity Column*Moment of Inertia Column)/(Effective Column Length^2)
Modulus of Elasticity given Rankine's Constant
​ Go Modulus of Elasticity Column = Column Crushing Stress/(pi^2*Rankine's Constant)
Rankine's Constant
​ Go Rankine's Constant = Column Crushing Stress/(pi^2*Modulus of Elasticity Column)
Ultimate Crushing Stress given Rankine's Constant
​ Go Column Crushing Stress = Rankine's Constant*pi^2*Modulus of Elasticity Column
Cross-Sectional Area of Column given Crushing Load
​ Go Column Cross Sectional Area = Crushing Load/Column Crushing Stress
Crushing Load given Ultimate Crushing Stress
​ Go Crushing Load = Column Crushing Stress*Column Cross Sectional Area
Ultimate Crushing Stress given Crushing Load
​ Go Column Crushing Stress = Crushing Load/Column Cross Sectional Area

14 Rankine's Formula Calculators

Effective Length of Column given Crippling Load and Rankine's Constant
​ Go Effective Column Length = sqrt((Column Crushing Stress*Column Cross Sectional Area/Crippling Load-1)*(Least Radius of Gyration Column^2)/Rankine's Constant)
Least Radius of Gyration given Crippling Load and Rankine's Constant
​ Go Least Radius of Gyration Column = sqrt((Rankine's Constant*Effective Column Length^2)/(Column Crushing Stress*Column Cross Sectional Area/Crippling Load-1))
Rankine's Constant given Crippling Load
​ Go Rankine's Constant = ((Column Crushing Stress*Column Cross Sectional Area)/Crippling Load-1)*((Least Radius of Gyration Column)/Effective Column Length)^2
Cross-Sectional Area of Column given Crippling Load and Rankine's Constant
​ Go Column Cross Sectional Area = (Crippling Load*(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2))/Column Crushing Stress
Ultimate Crushing Stress given Crippling Load and Rankine's Constant
​ Go Column Crushing Stress = (Crippling Load*(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2))/Column Cross Sectional Area
Crippling Load given Rankine's Constant
​ Go Crippling Load = (Column Crushing Stress*Column Cross Sectional Area)/(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2)
Crushing Load by Rankine's Formula
​ Go Crushing Load = (Rankine’s Critical Load*Euler’s Buckling Load)/(Euler’s Buckling Load-Rankine’s Critical Load)
Crippling Load by Rankine's Formula
​ Go Rankine’s Critical Load = (Crushing Load*Euler’s Buckling Load)/(Crushing Load+Euler’s Buckling Load)
Modulus of Elasticity given Rankine's Constant
​ Go Modulus of Elasticity Column = Column Crushing Stress/(pi^2*Rankine's Constant)
Rankine's Constant
​ Go Rankine's Constant = Column Crushing Stress/(pi^2*Modulus of Elasticity Column)
Ultimate Crushing Stress given Rankine's Constant
​ Go Column Crushing Stress = Rankine's Constant*pi^2*Modulus of Elasticity Column
Cross-Sectional Area of Column given Crushing Load
​ Go Column Cross Sectional Area = Crushing Load/Column Crushing Stress
Crushing Load given Ultimate Crushing Stress
​ Go Crushing Load = Column Crushing Stress*Column Cross Sectional Area
Ultimate Crushing Stress given Crushing Load
​ Go Column Crushing Stress = Crushing Load/Column Cross Sectional Area

Ultimate Crushing Stress given Crushing Load Formula

Column Crushing Stress = Crushing Load/Column Cross Sectional Area
σc = Pc/A

What is Ultimate Compressive Strength?

Ultimate Compressive Strength is defined as the force at which a specimen with a certain cross-section, and consisting of a particular fracturing material, fails when it is subjected to compression. The ultimate compressive strength is normally measured in N/mm2 (force per area) and is thus stress.

How to Calculate Ultimate Crushing Stress given Crushing Load?

Ultimate Crushing Stress given Crushing Load calculator uses Column Crushing Stress = Crushing Load/Column Cross Sectional Area to calculate the Column Crushing Stress, The Ultimate Crushing Stress given Crushing Load formula is defined as a special type of localized compressive stress which occurs at the surface of contact of two members that are relatively at rest. Column Crushing Stress is denoted by σc symbol.

How to calculate Ultimate Crushing Stress given Crushing Load using this online calculator? To use this online calculator for Ultimate Crushing Stress given Crushing Load, enter Crushing Load (Pc) & Column Cross Sectional Area (A) and hit the calculate button. Here is how the Ultimate Crushing Stress given Crushing Load calculation can be explained with given input values -> 1.1E-6 = 1500000/0.002.

FAQ

What is Ultimate Crushing Stress given Crushing Load?
The Ultimate Crushing Stress given Crushing Load formula is defined as a special type of localized compressive stress which occurs at the surface of contact of two members that are relatively at rest and is represented as σc = Pc/A or Column Crushing Stress = Crushing Load/Column Cross Sectional Area. Crushing Load is the intensity of load required to crush the material & 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 Ultimate Crushing Stress given Crushing Load?
The Ultimate Crushing Stress given Crushing Load formula is defined as a special type of localized compressive stress which occurs at the surface of contact of two members that are relatively at rest is calculated using Column Crushing Stress = Crushing Load/Column Cross Sectional Area. To calculate Ultimate Crushing Stress given Crushing Load, you need Crushing Load (Pc) & Column Cross Sectional Area (A). With our tool, you need to enter the respective value for Crushing 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.
How many ways are there to calculate Column Crushing Stress?
In this formula, Column Crushing Stress uses Crushing Load & Column Cross Sectional Area. We can use 4 other way(s) to calculate the same, which is/are as follows -
  • Column Crushing Stress = (Crippling Load*(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2))/Column Cross Sectional Area
  • Column Crushing Stress = Rankine's Constant*pi^2*Modulus of Elasticity Column
  • Column Crushing Stress = (Crippling Load*(1+Rankine's Constant*(Effective Column Length/Least Radius of Gyration Column)^2))/Column Cross Sectional Area
  • Column Crushing Stress = Rankine's Constant*pi^2*Modulus of Elasticity Column
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