Tensile radial strain for thick spherical shell Solution

STEP 0: Pre-Calculation Summary
Formula Used
Tensile Strain = ((Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value)
εtensile = ((Pv+(2*σθ/M))/F'c)
This formula uses 5 Variables
Variables Used
Tensile Strain - Tensile Strain is the ratio of change in length to original length.
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
εtensile = ((Pv+(2*σθ/M))/F'c) --> ((14000+(2*2000/35.45))/10000000)
Evaluating ... ...
εtensile = 0.00141128349788434
STEP 3: Convert Result to Output's Unit
0.00141128349788434 --> No Conversion Required
FINAL ANSWER
0.00141128349788434 0.001411 <-- Tensile 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

Tensile radial strain for thick spherical shell Formula

​LaTeX ​Go
Tensile Strain = ((Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value)
εtensile = ((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 Tensile radial strain for thick spherical shell?

Tensile radial strain for thick spherical shell calculator uses Tensile Strain = ((Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value) to calculate the Tensile Strain, Tensile radial strain for thick spherical shell formula is defined as a measure of the deformation experienced by a thick spherical shell under internal pressure and circumferential stress. It helps in understanding the material's response to applied loads, ensuring structural integrity and safety in engineering applications. Tensile Strain is denoted by εtensile symbol.

How to calculate Tensile radial strain for thick spherical shell using this online calculator? To use this online calculator for Tensile radial strain for thick spherical shell, 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 Tensile radial strain for thick spherical shell calculation can be explained with given input values -> 0.001411 = ((14000+(2*2000/35.45))/10000000).

FAQ

What is Tensile radial strain for thick spherical shell?
Tensile radial strain for thick spherical shell formula is defined as a measure of the deformation experienced by a thick spherical shell under internal pressure and circumferential stress. It helps in understanding the material's response to applied loads, ensuring structural integrity and safety in engineering applications and is represented as εtensile = ((Pv+(2*σθ/M))/F'c) or Tensile 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 Tensile radial strain for thick spherical shell?
Tensile radial strain for thick spherical shell formula is defined as a measure of the deformation experienced by a thick spherical shell under internal pressure and circumferential stress. It helps in understanding the material's response to applied loads, ensuring structural integrity and safety in engineering applications is calculated using Tensile Strain = ((Radial Pressure+(2*Hoop Stress on thick shell/Mass Of Shell))/Adjusted design value). To calculate Tensile radial strain for thick spherical shell, 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 Tensile Strain?
In this formula, Tensile 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 -
  • Tensile Strain = ((Radial Pressure+(2*Hoop Stress on thick shell*Poisson's Ratio))/Adjusted design value)
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