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Circumferential stress developed in pipe wall Solution

STEP 0: Pre-Calculation Summary
Formula Used
circumferential_stress = (Pressure*Diameter of Pipe)/(2*Thickness of pipe)
σc = (P*D)/(2*t)
This formula uses 3 Variables
Variables Used
Pressure - Pressure is the force applied perpendicular to the surface of an object per unit area over which that force is distributed. (Measured in Pascal)
Diameter of Pipe - Diameter of Pipe is the length of the longest chord of the pipe in which the liquid is flowing. (Measured in Centimeter)
Thickness of pipe - Thickness of pipe is the smaller dimention of pipe . (Measured in Meter)
STEP 1: Convert Input(s) to Base Unit
Pressure: 800 Pascal --> 800 Pascal No Conversion Required
Diameter of Pipe: 2 Centimeter --> 0.02 Meter (Check conversion here)
Thickness of pipe: 3 Meter --> 3 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σc = (P*D)/(2*t) --> (800*0.02)/(2*3)
Evaluating ... ...
σc = 2.66666666666667
STEP 3: Convert Result to Output's Unit
2.66666666666667 Pascal -->2.66666666666667 Newton per Square Meter (Check conversion here)
FINAL ANSWER
2.66666666666667 Newton per Square Meter <-- Circumferential stress
(Calculation completed in 00.016 seconds)

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difference_in_liquid_level = (4*Coefficient of Friction/(2*[g]))*((Length of pipe 1*Velocity at point 1^2/Diameter of pipe 1)+(Length of pipe 2*Velocity at point 2^2/Diameter of pipe 2)+(Length of pipe 3*Velocity at 3^2/Diameter of pipe 3)) Go
Power transmission through pipes
power_transmitted = (Density*[g]*pi*(Diameter of Pipe^2)*Flow Velocity/4000)*(Total Head at Entrance-(4*Coefficient of Friction*Length of Pipe*(Flow Velocity^2)/(Diameter of Pipe*2*[g]))) Go
Maximum area of obstruction in the pipe
maximum_area_of_obstruction = Cross sectional area of Pipe-((Cross sectional area of Pipe*Velocity of the fluid particle)/(Coefficient of contraction*Velocity of liquid vena contracta)) Go
Discharge in the equivalent pipe
discharge = sqrt((Loss of head*(pi^2)*2*(Diameter of Pipe^5)*[g])/(4*16*Coefficient of Friction*Length of Pipe)) Go
Coefficient of contraction for sudden contraction
coefficient_of_contraction = Velocity at section 2-2/(Velocity at section 2-2+sqrt(Loss of head sudden contraction*2*[g])) Go
Diameter of the equivalent pipe
diameter_of_pipe = ((4*16*(Discharge^2)*Coefficient of Friction*Length of Pipe)/((pi^2)*2*Loss of head*[g]))^(1/5) Go
Length of the equivalent pipe
length_of_pipe = (Loss of head*(pi^2)*2*(Diameter of Pipe^5)*[g])/(4*16*(Discharge^2)*Coefficient of Friction) Go
Area of the pipe for maximum power transmission through nozzle
area_of_pipe = Nozzle area at outlet*sqrt(8*Coefficient of Friction*Length of Pipe/Diameter of Pipe) Go
Power lost due to sudden enlargement
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Diameter of nozzle for maximum power transmission through nozzle
diameter_of_nozzle = ((Diameter of Pipe^5)/(8*Coefficient of Friction*Length of Pipe))^0.25 Go

Circumferential stress developed in pipe wall Formula

circumferential_stress = (Pressure*Diameter of Pipe)/(2*Thickness of pipe)
σc = (P*D)/(2*t)

What circumferential stress is developed in the pipe?

The circumferential stress, also known as tangential stress, in a tank or pipe can be determined by applying the concept of fluid pressure against curved surfaces. The wall of a tank or pipe carrying fluid under pressure is subjected to tensile forces across its longitudinal and transverse sections.

What is the difference between longitudinal and circumferential stress?

Circumferential stress is the stress acting along the circumferential direction, it is generally tensile in nature. Longitudinal stress is the stress which acts along the length and it is also tensile in nature whereas radial stress which acts in the direction of the radius is compressive in nature.

How to Calculate Circumferential stress developed in pipe wall?

Circumferential stress developed in pipe wall calculator uses circumferential_stress = (Pressure*Diameter of Pipe)/(2*Thickness of pipe) to calculate the Circumferential stress, The Circumferential stress developed in pipe wall formula is defined as the ratio of pressure & diameter to thickness of the pipe. Circumferential stress is denoted by σc symbol.

How to calculate Circumferential stress developed in pipe wall using this online calculator? To use this online calculator for Circumferential stress developed in pipe wall, enter Pressure (P), Diameter of Pipe (D) & Thickness of pipe (t) and hit the calculate button. Here is how the Circumferential stress developed in pipe wall calculation can be explained with given input values -> 2.666667 = (800*0.02)/(2*3).

FAQ

What is Circumferential stress developed in pipe wall?
The Circumferential stress developed in pipe wall formula is defined as the ratio of pressure & diameter to thickness of the pipe and is represented as σc = (P*D)/(2*t) or circumferential_stress = (Pressure*Diameter of Pipe)/(2*Thickness of pipe). Pressure is the force applied perpendicular to the surface of an object per unit area over which that force is distributed, Diameter of Pipe is the length of the longest chord of the pipe in which the liquid is flowing & Thickness of pipe is the smaller dimention of pipe .
How to calculate Circumferential stress developed in pipe wall?
The Circumferential stress developed in pipe wall formula is defined as the ratio of pressure & diameter to thickness of the pipe is calculated using circumferential_stress = (Pressure*Diameter of Pipe)/(2*Thickness of pipe). To calculate Circumferential stress developed in pipe wall, you need Pressure (P), Diameter of Pipe (D) & Thickness of pipe (t). With our tool, you need to enter the respective value for Pressure, Diameter of Pipe & Thickness of pipe 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 stress?
In this formula, Circumferential stress uses Pressure, Diameter of Pipe & Thickness of pipe. We can use 10 other way(s) to calculate the same, which is/are as follows -
  • maximum_area_of_obstruction = Cross sectional area of Pipe-((Cross sectional area of Pipe*Velocity of the fluid particle)/(Coefficient of contraction*Velocity of liquid vena contracta))
  • discharge = sqrt((Loss of head*(pi^2)*2*(Diameter of Pipe^5)*[g])/(4*16*Coefficient of Friction*Length of Pipe))
  • diameter_of_pipe = ((4*16*(Discharge^2)*Coefficient of Friction*Length of Pipe)/((pi^2)*2*Loss of head*[g]))^(1/5)
  • length_of_pipe = (Loss of head*(pi^2)*2*(Diameter of Pipe^5)*[g])/(4*16*(Discharge^2)*Coefficient of Friction)
  • difference_in_liquid_level = (4*Coefficient of Friction/(2*[g]))*((Length of pipe 1*Velocity at point 1^2/Diameter of pipe 1)+(Length of pipe 2*Velocity at point 2^2/Diameter of pipe 2)+(Length of pipe 3*Velocity at 3^2/Diameter of pipe 3))
  • power = (Density of Fluid*[g]*Discharge*Loss of head sudden enlargement)/1000
  • coefficient_of_contraction = Velocity at section 2-2/(Velocity at section 2-2+sqrt(Loss of head sudden contraction*2*[g]))
  • power_transmitted = (Density*[g]*pi*(Diameter of Pipe^2)*Flow Velocity/4000)*(Total Head at Entrance-(4*Coefficient of Friction*Length of Pipe*(Flow Velocity^2)/(Diameter of Pipe*2*[g])))
  • diameter_of_nozzle = ((Diameter of Pipe^5)/(8*Coefficient of Friction*Length of Pipe))^0.25
  • area_of_pipe = Nozzle area at outlet*sqrt(8*Coefficient of Friction*Length of Pipe/Diameter of Pipe)
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