Longitudinal Stress (Axial Stress) in Cylindrical Shell Solution

STEP 0: Pre-Calculation Summary
Formula Used
Longitudinal Stress for Cylindrical Shell = (Internal Pressure given Longitudinal Stress*Mean Diameter of Shell)/4*Thickness of Cylindrical Shell
σCylindricalShell = (PLS*D)/4*tc
This formula uses 4 Variables
Variables Used
Longitudinal Stress for Cylindrical Shell - (Measured in Pascal) - Longitudinal Stress for Cylindrical Shell refers to the stress acting parallel to the longitudinal axis of the cylinder.
Internal Pressure given Longitudinal Stress - (Measured in Pascal) - Internal Pressure given Longitudinal Stress is a measure of how the internal energy of a system changes when it expands or contracts at a constant temperature.
Mean Diameter of Shell - (Measured in Meter) - Mean Diameter of Shell is the average of two measurements of the diameter taken at right angles to each other.
Thickness of Cylindrical Shell - (Measured in Meter) - The Thickness of Cylindrical Shell is based on simplified stress analysis and allowable stress for the material of construction.
STEP 1: Convert Input(s) to Base Unit
Internal Pressure given Longitudinal Stress: 51776.64 Pascal --> 51776.64 Pascal No Conversion Required
Mean Diameter of Shell: 5 Meter --> 5 Meter No Conversion Required
Thickness of Cylindrical Shell: 2.4 Meter --> 2.4 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σCylindricalShell = (PLS*D)/4*tc --> (51776.64*5)/4*2.4
Evaluating ... ...
σCylindricalShell = 155329.92
STEP 3: Convert Result to Output's Unit
155329.92 Pascal --> No Conversion Required
FINAL ANSWER
155329.92 155329.9 Pascal <-- Longitudinal Stress for Cylindrical Shell
(Calculation completed in 00.004 seconds)

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17 Design of Pressure Vessel Subjected to Internal Pressure Calculators

Coefficient Value for Thickness of Flange
Go Coefficient Value for Thickness of Flange = ((1)/((0.3)+(1.5*Maximum Bolt Loads*Radial Distance)/(Hydrostatic End Force in Gasket Seal*Diameter of Gasket at Load Reaction)))
Gasket Factor
Go Gasket Factor = (Total Fastener Force-Inside Area of Gasket*Test Pressure)/(Gasket Area*Test Pressure)
Longitudinal Stress (Axial Stress) in Cylindrical Shell
Go Longitudinal Stress for Cylindrical Shell = (Internal Pressure given Longitudinal Stress*Mean Diameter of Shell)/4*Thickness of Cylindrical Shell
Internal Presure of Vessel given Longitudinal Stress
Go Internal Pressure given Longitudinal Stress = (4*Longitudinal Stress*Thickness of Cylindrical Shell)/(Mean Diameter of Shell)
Wall Thickness of Pressure Vessel given Longitudinal Stress
Go Thickness of Shell for Longitudinal Stress = (Internal Pressure for Vessel*Mean Diameter of Shell)/(4*Longitudinal Stress)
Wall Thickness of Cylindrical Shell Given Hoop Stress
Go Thickness of Shell for Hoop Stress = (2*Internal Pressure given Hoop Stress*Mean Diameter of Shell)/Circumferential Stress
Internal Pressure of Cylindrical Vessel given Hoop Stress
Go Internal Pressure given Hoop Stress = (2*Circumferential Stress*Thickness of Cylindrical Shell)/(Mean Diameter of Shell)
Circumferential Stress (Hoop Stress) in Cylinderical Shell
Go Circumferential Stress = (Internal Pressure for Vessel*Mean Diameter of Shell)/2*Thickness of Cylindrical Shell
Maximum Bolt Spacing
Go Maximum Bolt Spacing = 2*Nominal Bolt Diameter+(6*Thickness of Flange/Gasket Factor+0.5)
Hydrostatic End Force using Design Pressure
Go Hydrostatic End Force = (pi/4)*(Radial Distance^2)*Internal Pressure
Diameter of Gasket at Load Reaction
Go Diameter of Gasket at Load Reaction = Outside Diameter of Gasket-2*Effective Gasket Seating Width
Effective Thickness of Conical Head
Go Effective Thickness = Thickness of Conical Head*(cos(Apex Angle))
Hoop Strain
Go Hoop Strain = (Final Length-Initial Length)/(Initial Length)
Radial Distance from Gasket Load Reaction to Bolt Circle
Go Radial Distance = (Bolt Circle Diameter-Diameter of Gasket at Load Reaction)/2
Bolt Circle Diameter
Go Bolt Circle Diameter = Outside Diameter of Gasket+(2*Nominal Bolt Diameter)+12
Outside Diameter of Flange using Bolt Diameter
Go Outside Flange Diameter = Bolt Circle Diameter+2*Nominal Bolt Diameter+12
Minimum Bolt Spacing
Go Minimum Bolt Spacing = 2.5*Nominal Bolt Diameter

Longitudinal Stress (Axial Stress) in Cylindrical Shell Formula

Longitudinal Stress for Cylindrical Shell = (Internal Pressure given Longitudinal Stress*Mean Diameter of Shell)/4*Thickness of Cylindrical Shell
σCylindricalShell = (PLS*D)/4*tc

What is Stress?

Stress is a quantity that describes the magnitude of forces that cause deformation. When forces pull on an object and cause its elongation, like the stretching of an elastic band, we call such stress a tensile stress. When forces cause a compression of an object, we call it a compressive stress. When an object is being squeezed from all sides, like a submarine in the depths of an ocean, we call this kind of stress a bulk stress (or volume stress).

How to Calculate Longitudinal Stress (Axial Stress) in Cylindrical Shell?

Longitudinal Stress (Axial Stress) in Cylindrical Shell calculator uses Longitudinal Stress for Cylindrical Shell = (Internal Pressure given Longitudinal Stress*Mean Diameter of Shell)/4*Thickness of Cylindrical Shell to calculate the Longitudinal Stress for Cylindrical Shell, Longitudinal Stress (Axial Stress) in Cylindrical shell is the result of a force acting perpendicular to an area of a body, causing the extension or compression of the material. Longitudinal Stress for Cylindrical Shell is denoted by σCylindricalShell symbol.

How to calculate Longitudinal Stress (Axial Stress) in Cylindrical Shell using this online calculator? To use this online calculator for Longitudinal Stress (Axial Stress) in Cylindrical Shell, enter Internal Pressure given Longitudinal Stress (PLS), Mean Diameter of Shell (D) & Thickness of Cylindrical Shell (tc) and hit the calculate button. Here is how the Longitudinal Stress (Axial Stress) in Cylindrical Shell calculation can be explained with given input values -> 155329.9 = (51776.64*5)/4*2.4.

FAQ

What is Longitudinal Stress (Axial Stress) in Cylindrical Shell?
Longitudinal Stress (Axial Stress) in Cylindrical shell is the result of a force acting perpendicular to an area of a body, causing the extension or compression of the material and is represented as σCylindricalShell = (PLS*D)/4*tc or Longitudinal Stress for Cylindrical Shell = (Internal Pressure given Longitudinal Stress*Mean Diameter of Shell)/4*Thickness of Cylindrical Shell. Internal Pressure given Longitudinal Stress is a measure of how the internal energy of a system changes when it expands or contracts at a constant temperature, Mean Diameter of Shell is the average of two measurements of the diameter taken at right angles to each other & The Thickness of Cylindrical Shell is based on simplified stress analysis and allowable stress for the material of construction.
How to calculate Longitudinal Stress (Axial Stress) in Cylindrical Shell?
Longitudinal Stress (Axial Stress) in Cylindrical shell is the result of a force acting perpendicular to an area of a body, causing the extension or compression of the material is calculated using Longitudinal Stress for Cylindrical Shell = (Internal Pressure given Longitudinal Stress*Mean Diameter of Shell)/4*Thickness of Cylindrical Shell. To calculate Longitudinal Stress (Axial Stress) in Cylindrical Shell, you need Internal Pressure given Longitudinal Stress (PLS), Mean Diameter of Shell (D) & Thickness of Cylindrical Shell (tc). With our tool, you need to enter the respective value for Internal Pressure given Longitudinal Stress, Mean Diameter of Shell & Thickness of Cylindrical 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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