Circumferential strain given stresses on cylindrical shell and Poisson's ratio Solution

STEP 0: Pre-Calculation Summary
Formula Used
Circumferential strain = (Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell
e1 = (σθ-(𝛎*(σl-σc)))/E
This formula uses 6 Variables
Variables Used
Circumferential strain - Circumferential strain represents the change in length.
Hoop Stress on thick shell - (Measured in Pascal) - Hoop Stress on thick shell is the circumferential stress in a cylinder.
Poisson's Ratio - Poisson's Ratio is defined as the ratio of the lateral and axial strain. For many metals and alloys, values of Poisson’s ratio range between 0.1 and 0.5.
Longitudinal Stress Thick Shell - (Measured in Pascal) - Longitudinal Stress Thick Shell is defined as the stress produced when a pipe is subjected to internal pressure.
Compressive Stress Thick Shell - (Measured in Pascal) - Compressive Stress Thick Shell is the force that is responsible for the deformation of the material such that the volume of the material reduces.
Modulus of Elasticity Of Thick Shell - (Measured in Pascal) - Modulus of Elasticity Of Thick Shell is a quantity that measures an object or substance's resistance to being deformed elastically when a stress is applied to it.
STEP 1: Convert Input(s) to Base Unit
Hoop Stress on thick shell: 0.002 Megapascal --> 2000 Pascal (Check conversion here)
Poisson's Ratio: 0.3 --> No Conversion Required
Longitudinal Stress Thick Shell: 0.08 Megapascal --> 80000 Pascal (Check conversion here)
Compressive Stress Thick Shell: 0.55 Megapascal --> 550000 Pascal (Check conversion here)
Modulus of Elasticity Of Thick Shell: 2.6 Megapascal --> 2600000 Pascal (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
e1 = (σθ-(𝛎*(σlc)))/E --> (2000-(0.3*(80000-550000)))/2600000
Evaluating ... ...
e1 = 0.055
STEP 3: Convert Result to Output's Unit
0.055 --> No Conversion Required
FINAL ANSWER
0.055 <-- Circumferential strain
(Calculation completed in 00.020 seconds)

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25 Stresses in Thick Cylindrical Shell Calculators

Poisson's ratio given longitudinal strain in thick cylindrical shell
Go Poisson's Ratio = Hoop Stress on thick shell-((Longitudinal Stress Thick Shell-(Longitudinal Strain*Modulus of Elasticity Of Thick Shell))/(Hoop Stress on thick shell-Compressive Stress Thick Shell))
Radius of thick cylindrical shell given stress on cylindrical shell and Poisson's ratio
Go Radius Of Cylindrical Shell = Change in radius/((Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell)
Change in radius of thick cylindrical shell given stresses and poison's ratio
Go Change in radius = Radius Of Cylindrical Shell*((Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell)
Modulus of elasticity given change in radius of thick cylindrical shell
Go Modulus of Elasticity Of Thick Shell = Radius Of Cylindrical Shell*((Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Change in radius)
Longitudinal stress given change in radius of thick cylindrical shell
Go Longitudinal Stress Thick Shell = ((Hoop Stress on thick shell-(Change in radius*Modulus of Elasticity Of Thick Shell/Radius Of Cylindrical Shell))/(Poisson's Ratio))+Compressive Stress Thick Shell
Compressive stress given change in radius of thick cylindrical shell
Go Compressive Stress Thick Shell = Longitudinal Stress Thick Shell-((Hoop Stress on thick shell-(Change in radius*Modulus of Elasticity Of Thick Shell/Radius Of Cylindrical Shell))/(Poisson's Ratio))
Poisson's ratio given change in radius of thick cylindrical shell
Go Poisson's Ratio = ((Hoop Stress on thick shell-(Change in radius*Modulus of Elasticity Of Thick Shell/Radius Of Cylindrical Shell))/(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell))
Circumferential stress given change in radius of thick cylindrical shell
Go Hoop Stress on thick shell = (Change in radius*Modulus of Elasticity Of Thick Shell/Radius Of Cylindrical Shell)+(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell))
Longitudinal stress given circumferential strain in thick cylindrical shell
Go Longitudinal Stress Thick Shell = ((Hoop Stress on thick shell-(Circumferential strain*Modulus of Elasticity Of Thick Shell))/(Poisson's Ratio))+Compressive Stress Thick Shell
Compressive stress given circumferential strain in thick cylindrical shell
Go Compressive Stress Thick Shell = Longitudinal Stress Thick Shell-((Hoop Stress on thick shell-(Circumferential strain*Modulus of Elasticity Of Thick Shell))/(Poisson's Ratio))
Circumferential strain given stresses on cylindrical shell and Poisson's ratio
Go Circumferential strain = (Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell
Circumferential stress given circumferential strain in thick cylindrical shell
Go Hoop Stress on thick shell = (Circumferential strain*Modulus of Elasticity Of Thick Shell)+(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell))
Modulus of elasticity given circumferential strain in thick cylindrical shell
Go Modulus of Elasticity Of Thick Shell = (Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Circumferential strain
Poisson's ratio given circumferential strain in thick cylindrical shell
Go Poisson's Ratio = ((Hoop Stress Thick Shell-(Circumferential strain*Modulus of Elasticity Of Thick Shell))/(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell))
Longitudinal strain given stresses in thick cylindrical shell and Poisson's ratio
Go Longitudinal Strain = (Longitudinal Stress Thick Shell-(Poisson's Ratio*(Hoop Stress on thick shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell
Circumferential stress given longitudinal strain in thick cylindrical shell
Go Hoop Stress on thick shell = ((Longitudinal Stress Thick Shell-(Longitudinal Strain*Modulus of Elasticity Of Thick Shell))/Poisson's Ratio)+Compressive Stress Thick Shell
Modulus of elasticity given longitudinal strain in thick cylindrical shell
Go Modulus of Elasticity Of Thick Shell = (Longitudinal Stress Thick Shell-(Poisson's Ratio*(Hoop Stress on thick shell-Compressive Stress Thick Shell)))/Longitudinal Strain
Longitudinal stress given longitudinal strain in thick cylindrical shell
Go Longitudinal Stress Thick Shell = (Longitudinal Strain*Modulus of Elasticity Of Thick Shell)+(Poisson's Ratio*(Hoop Stress on thick shell-Compressive Stress Thick Shell))
Compressive stress given longitudinal strain in thick cylindrical shell
Go Compressive Stress Thick Shell = Hoop Stress on thick shell-((Longitudinal Stress Thick Shell-(Longitudinal Strain*Modulus of Elasticity Of Thick Shell))/Poisson's Ratio)
Circumferential stress given radial strain in thick cylindrical shell
Go Hoop Stress on thick shell = ((-Compressive Stress Thick Shell-(Strain*Modulus of Elasticity Of Thick Shell))/Poisson's Ratio)-Longitudinal Stress Thick Shell
Modulus of elasticity given radial strain in thick cylindrical shell
Go Modulus of Elasticity Of Thick Shell = (-Compressive Stress Thick Shell-(Poisson's Ratio*(Hoop Stress on thick shell+Longitudinal Stress Thick Shell)))/Strain
Radial strain given stresses on thick cylinder and poisson's ratio
Go Strain = (-Compressive Stress Thick Shell-(Poisson's Ratio*(Hoop Stress on thick shell+Longitudinal Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell
Longitudinal stress given radial strain in thick cylindrical shell
Go Longitudinal Stress Thick Shell = ((-Compressive Stress Thick Shell-(Strain*Modulus of Elasticity Of Thick Shell))/Poisson's Ratio)-Hoop Stress on thick shell
Compressive stress given radial strain in thick cylindrical shell
Go Compressive Stress Thick Shell = -(Strain*Modulus of Elasticity Of Thick Shell)-(Poisson's Ratio*(Hoop Stress on thick shell+Longitudinal Stress Thick Shell))
Poisson's ratio given radial strain in thick cylindrical shell
Go Poisson's Ratio = (-Compressive Stress Thick Shell-(Strain*Modulus of Elasticity Of Thick Shell))/(Hoop Stress on thick shell+Longitudinal Stress Thick Shell)

Circumferential strain given stresses on cylindrical shell and Poisson's ratio Formula

Circumferential strain = (Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell
e1 = (σθ-(𝛎*(σl-σc)))/E

What is the strain in physics?

Strain is simply the measure of how much an object is stretched or deformed. A strain occurs when force is applied to an object. Strain deals mostly with the change in length of the object.

How to Calculate Circumferential strain given stresses on cylindrical shell and Poisson's ratio?

Circumferential strain given stresses on cylindrical shell and Poisson's ratio calculator uses Circumferential strain = (Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell to calculate the Circumferential strain, The Circumferential strain given stresses on cylindrical shell and Poisson's ratio formula represents the change in length. Circumferential strain is denoted by e1 symbol.

How to calculate Circumferential strain given stresses on cylindrical shell and Poisson's ratio using this online calculator? To use this online calculator for Circumferential strain given stresses on cylindrical shell and Poisson's ratio, enter Hoop Stress on thick shell θ), Poisson's Ratio (𝛎), Longitudinal Stress Thick Shell l), Compressive Stress Thick Shell c) & Modulus of Elasticity Of Thick Shell (E) and hit the calculate button. Here is how the Circumferential strain given stresses on cylindrical shell and Poisson's ratio calculation can be explained with given input values -> 0.055 = (2000-(0.3*(80000-550000)))/2600000.

FAQ

What is Circumferential strain given stresses on cylindrical shell and Poisson's ratio?
The Circumferential strain given stresses on cylindrical shell and Poisson's ratio formula represents the change in length and is represented as e1 = (σθ-(𝛎*(σlc)))/E or Circumferential strain = (Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell. Hoop Stress on thick shell is the circumferential stress in a cylinder, Poisson's Ratio is defined as the ratio of the lateral and axial strain. For many metals and alloys, values of Poisson’s ratio range between 0.1 and 0.5, Longitudinal Stress Thick Shell is defined as the stress produced when a pipe is subjected to internal pressure, Compressive Stress Thick Shell is the force that is responsible for the deformation of the material such that the volume of the material reduces & Modulus of Elasticity Of Thick Shell is a quantity that measures an object or substance's resistance to being deformed elastically when a stress is applied to it.
How to calculate Circumferential strain given stresses on cylindrical shell and Poisson's ratio?
The Circumferential strain given stresses on cylindrical shell and Poisson's ratio formula represents the change in length is calculated using Circumferential strain = (Hoop Stress on thick shell-(Poisson's Ratio*(Longitudinal Stress Thick Shell-Compressive Stress Thick Shell)))/Modulus of Elasticity Of Thick Shell. To calculate Circumferential strain given stresses on cylindrical shell and Poisson's ratio, you need Hoop Stress on thick shell θ), Poisson's Ratio (𝛎), Longitudinal Stress Thick Shell l), Compressive Stress Thick Shell c) & Modulus of Elasticity Of Thick Shell (E). With our tool, you need to enter the respective value for Hoop Stress on thick shell, Poisson's Ratio, Longitudinal Stress Thick Shell, Compressive Stress Thick Shell & Modulus of Elasticity Of Thick Shell 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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