Circumferential strain given volumetric strain for thin cylindrical shell Solution

STEP 0: Pre-Calculation Summary
Formula Used
Circumferential Strain Thin Shell = (Volumetric Strain-Longitudinal Strain)/2
e1 = (εv-εlongitudinal)/2
This formula uses 3 Variables
Variables Used
Circumferential Strain Thin Shell - Circumferential strain Thin Shell represents the change in length.
Volumetric Strain - The Volumetric Strain is the ratio of change in volume to original volume.
Longitudinal Strain - The Longitudinal Strain is ratio of change in length to original length.
STEP 1: Convert Input(s) to Base Unit
Volumetric Strain: 46 --> No Conversion Required
Longitudinal Strain: 40 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
e1 = (εvlongitudinal)/2 --> (46-40)/2
Evaluating ... ...
e1 = 3
STEP 3: Convert Result to Output's Unit
3 --> No Conversion Required
FINAL ANSWER
3 <-- Circumferential Strain Thin Shell
(Calculation completed in 00.004 seconds)

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National Institute Of Technology (NIT), Hamirpur
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Birsa Institute of Technology (BIT), Sindri
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Circumferential strain given internal fluid pressure
​ LaTeX ​ Go Circumferential Strain Thin Shell = ((Internal Pressure in thin shell*Inner Diameter of Cylinder)/(2*Thickness Of Thin Shell*Modulus of Elasticity Of Thin Shell))*((1/2)-Poisson's Ratio)
Longitudinal strain in thin cylindrical vessel given internal fluid pressure
​ LaTeX ​ Go Longitudinal Strain = ((Internal Pressure in thin shell*Inner Diameter of Cylinder)/(2*Thickness Of Thin Shell*Modulus of Elasticity Of Thin Shell))*((1/2)-Poisson's Ratio)
Circumferential strain given hoop stress
​ LaTeX ​ Go Circumferential Strain Thin Shell = (Hoop Stress in Thin shell-(Poisson's Ratio*Longitudinal Stress Thick Shell))/Modulus of Elasticity Of Thin Shell
Longitudinal strain given hoop and longitudinal stress
​ LaTeX ​ Go Longitudinal Strain = (Longitudinal Stress Thick Shell-(Poisson's Ratio*Hoop Stress in Thin shell))/Modulus of Elasticity Of Thin Shell

Strain Calculators

Strain in thin spherical shell given internal fluid pressure
​ LaTeX ​ Go Strain in thin shell = ((Internal Pressure*Diameter of Sphere)/(4*Thickness Of Thin Spherical Shell*Modulus of Elasticity Of Thin Shell))*(1-Poisson's Ratio)
Circumferential strain given hoop stress
​ LaTeX ​ Go Circumferential Strain Thin Shell = (Hoop Stress in Thin shell-(Poisson's Ratio*Longitudinal Stress Thick Shell))/Modulus of Elasticity Of Thin Shell
Strain in any one direction of thin spherical shell
​ LaTeX ​ Go Strain in thin shell = (Hoop Stress in Thin shell/Modulus of Elasticity Of Thin Shell)*(1-Poisson's Ratio)
Circumferential strain given circumference
​ LaTeX ​ Go Circumferential Strain Thin Shell = Change in Circumference/Original Circumference

Circumferential strain given volumetric strain for thin cylindrical shell Formula

​LaTeX ​Go
Circumferential Strain Thin Shell = (Volumetric Strain-Longitudinal Strain)/2
e1 = (εv-εlongitudinal)/2

What is the relation between lateral strain and longitudinal strain?

Lateral strain is defined as the ratio of decrease in the length of the bar in the perpendicular direction of applied load to that of the original length (gauge length). Poisson's ratio: The ratio of lateral strain to that of the longitudinal strain is termed as Poisson's ratio and it is represented by ϻ or 1/m.

How to Calculate Circumferential strain given volumetric strain for thin cylindrical shell?

Circumferential strain given volumetric strain for thin cylindrical shell calculator uses Circumferential Strain Thin Shell = (Volumetric Strain-Longitudinal Strain)/2 to calculate the Circumferential Strain Thin Shell, The Circumferential strain given volumetric strain for thin cylindrical shell formula is defined as the change in length (shortening in systole, represented as a negative strain value) of the myocardium along the circumferential axis of the LV as viewed in the short axis. Circumferential Strain Thin Shell is denoted by e1 symbol.

How to calculate Circumferential strain given volumetric strain for thin cylindrical shell using this online calculator? To use this online calculator for Circumferential strain given volumetric strain for thin cylindrical shell, enter Volumetric Strain v) & Longitudinal Strain longitudinal) and hit the calculate button. Here is how the Circumferential strain given volumetric strain for thin cylindrical shell calculation can be explained with given input values -> -5 = (46-40)/2.

FAQ

What is Circumferential strain given volumetric strain for thin cylindrical shell?
The Circumferential strain given volumetric strain for thin cylindrical shell formula is defined as the change in length (shortening in systole, represented as a negative strain value) of the myocardium along the circumferential axis of the LV as viewed in the short axis and is represented as e1 = (εvlongitudinal)/2 or Circumferential Strain Thin Shell = (Volumetric Strain-Longitudinal Strain)/2. The Volumetric Strain is the ratio of change in volume to original volume & The Longitudinal Strain is ratio of change in length to original length.
How to calculate Circumferential strain given volumetric strain for thin cylindrical shell?
The Circumferential strain given volumetric strain for thin cylindrical shell formula is defined as the change in length (shortening in systole, represented as a negative strain value) of the myocardium along the circumferential axis of the LV as viewed in the short axis is calculated using Circumferential Strain Thin Shell = (Volumetric Strain-Longitudinal Strain)/2. To calculate Circumferential strain given volumetric strain for thin cylindrical shell, you need Volumetric Strain v) & Longitudinal Strain longitudinal). With our tool, you need to enter the respective value for Volumetric Strain & Longitudinal Strain 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 Circumferential Strain Thin Shell?
In this formula, Circumferential Strain Thin Shell uses Volumetric Strain & Longitudinal Strain. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Circumferential Strain Thin Shell = (Hoop Stress in Thin shell-(Poisson's Ratio*Longitudinal Stress Thick Shell))/Modulus of Elasticity Of Thin Shell
  • Circumferential Strain Thin Shell = ((Internal Pressure in thin shell*Inner Diameter of Cylinder)/(2*Thickness Of Thin Shell*Modulus of Elasticity Of Thin Shell))*((1/2)-Poisson's Ratio)
  • Circumferential Strain Thin Shell = Change in Circumference/Original Circumference
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