Compressive radial strain for thick spherical shells Solution

STEP 0: Pre-Calculation Summary
Formula Used
Compressive Strain = (Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value
εcompressive = (Pv+(2*σθ/M))/F'c
This formula uses 5 Variables
Variables Used
Compressive Strain - The Compressive Strain is the ratio of change in length to the original length of the body when subjected to a compressive load.
Radial Pressure - (Measured in Pascal per Square Meter) - Radial Pressure is pressure towards or away from the central axis of a component.
Hoop Stress on thick shell - (Measured in Pascal) - Hoop Stress on thick shell is the circumferential stress in a cylinder.
Mass Of Shell - (Measured in Kilogram) - Mass Of Shell is the quantity of matter in a body regardless of its volume or of any forces acting on it.
Adjusted design value - (Measured in Pascal) - Adjusted design value for compression corrects the design value by using some factor.
STEP 1: Convert Input(s) to Base Unit
Radial Pressure: 0.014 Megapascal per Square Meter --> 14000 Pascal per Square Meter (Check conversion ​here)
Hoop Stress on thick shell: 0.002 Megapascal --> 2000 Pascal (Check conversion ​here)
Mass Of Shell: 35.45 Kilogram --> 35.45 Kilogram No Conversion Required
Adjusted design value: 10 Megapascal --> 10000000 Pascal (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
εcompressive = (Pv+(2*σθ/M))/F'c --> (14000+(2*2000/35.45))/10000000
Evaluating ... ...
εcompressive = 0.00141128349788434
STEP 3: Convert Result to Output's Unit
0.00141128349788434 --> No Conversion Required
FINAL ANSWER
0.00141128349788434 0.001411 <-- Compressive Strain
(Calculation completed in 00.004 seconds)

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Thick Spherical Shells Calculators

Mass of thick spherical shell given compressive radial strain
​ LaTeX ​ Go Mass Of Shell = (2*Hoop Stress on thick shell)/((Modulus of Elasticity Of Thick Shell*Compressive Strain)-Radial Pressure)
Hoop stress on thick spherical shell given compressive radial strain
​ LaTeX ​ Go Hoop Stress on thick shell = ((Modulus of Elasticity Of Thick Shell*Compressive Strain)-Radial Pressure)*Mass Of Shell/2
Radial pressure on thick spherical shell given compressive radial strain
​ LaTeX ​ Go Radial Pressure = (Adjusted design value*Compressive Strain)-(2*Hoop Stress on thick shell/Mass Of Shell)
Compressive radial strain for thick spherical shells
​ LaTeX ​ Go Compressive Strain = (Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value

Compressive radial strain for thick spherical shells Formula

​LaTeX ​Go
Compressive Strain = (Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value
εcompressive = (Pv+(2*σθ/M))/F'c

What is meant by hoop stress?

The hoop stress is the force over the area exerted circumferentially (perpendicular to the axis and the radius of the object) in both directions on every particle in the cylinder wall.

How to Calculate Compressive radial strain for thick spherical shells?

Compressive radial strain for thick spherical shells calculator uses Compressive Strain = (Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value to calculate the Compressive Strain, Compressive radial strain for thick spherical shells formula is defined as a measure of the deformation experienced by a thick spherical shell under internal pressure and external forces. It helps in understanding the material behavior and structural integrity of spherical shells in engineering applications. Compressive Strain is denoted by εcompressive symbol.

How to calculate Compressive radial strain for thick spherical shells using this online calculator? To use this online calculator for Compressive radial strain for thick spherical shells, enter Radial Pressure (Pv), Hoop Stress on thick shell θ), Mass Of Shell (M) & Adjusted design value (F'c) and hit the calculate button. Here is how the Compressive radial strain for thick spherical shells calculation can be explained with given input values -> 0.001411 = (14000+(2*2000/35.45))/10000000.

FAQ

What is Compressive radial strain for thick spherical shells?
Compressive radial strain for thick spherical shells formula is defined as a measure of the deformation experienced by a thick spherical shell under internal pressure and external forces. It helps in understanding the material behavior and structural integrity of spherical shells in engineering applications and is represented as εcompressive = (Pv+(2*σθ/M))/F'c or Compressive Strain = (Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value. Radial Pressure is pressure towards or away from the central axis of a component, Hoop Stress on thick shell is the circumferential stress in a cylinder, Mass Of Shell is the quantity of matter in a body regardless of its volume or of any forces acting on it & Adjusted design value for compression corrects the design value by using some factor.
How to calculate Compressive radial strain for thick spherical shells?
Compressive radial strain for thick spherical shells formula is defined as a measure of the deformation experienced by a thick spherical shell under internal pressure and external forces. It helps in understanding the material behavior and structural integrity of spherical shells in engineering applications is calculated using Compressive Strain = (Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value. To calculate Compressive radial strain for thick spherical shells, you need Radial Pressure (Pv), Hoop Stress on thick shell θ), Mass Of Shell (M) & Adjusted design value (F'c). With our tool, you need to enter the respective value for Radial Pressure, Hoop Stress on thick shell, Mass Of Shell & Adjusted design value 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 Compressive Strain?
In this formula, Compressive Strain uses Radial Pressure, Hoop Stress on thick shell, Mass Of Shell & Adjusted design value. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Compressive Strain = (Radial Pressure+(2*Hoop Stress on thick shell*Poisson's Ratio))/Adjusted design value
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