Thickness of Jacket Shell for Internal Pressure Solution

STEP 0: Pre-Calculation Summary
Formula Used
Required Thickness of Jacket = (Design Jacket Pressure*Internal Diameter of Shell)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell)-Design Jacket Pressure)
trj = (pj*Di)/((2*fj*J)-pj)
This formula uses 5 Variables
Variables Used
Required Thickness of Jacket - (Measured in Millimeter) - Required Thickness of Jacket refers to the thickness of the outer shell of a vessel that surrounds the main vessel and is used to provide heating or cooling to the contents of the vessel.
Design Jacket Pressure - (Measured in Newton per Square Millimeter) - Design Jacket Pressure refers to a type of pressure vessel designed to withstand high pressures and temperatures, typically used for containing gases or liquids under extreme conditions.
Internal Diameter of Shell - (Measured in Millimeter) - Internal Diameter of Shell is a measurement of the distance of a straight line from one point on the inner wall of the object, through its center, to an opposite point also on the inside.
Allowable Stress for Jacket Material - (Measured in Newton per Square Millimeter) - Allowable Stress for Jacket Material at Design Temperature is defined as the material failure stress divided by a factor of safety greater than one.
Joint Efficiency for Shell - Joint Efficiency for Shell refers to the effectiveness of the joint between two adjacent sections of a cylindrical shell, such as in a pressure vessel or a storage tank.
STEP 1: Convert Input(s) to Base Unit
Design Jacket Pressure: 0.105 Newton per Square Millimeter --> 0.105 Newton per Square Millimeter No Conversion Required
Internal Diameter of Shell: 1500 Millimeter --> 1500 Millimeter No Conversion Required
Allowable Stress for Jacket Material: 120 Newton per Square Millimeter --> 120 Newton per Square Millimeter No Conversion Required
Joint Efficiency for Shell: 0.85 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
trj = (pj*Di)/((2*fj*J)-pj) --> (0.105*1500)/((2*120*0.85)-0.105)
Evaluating ... ...
trj = 0.772456411388215
STEP 3: Convert Result to Output's Unit
0.000772456411388215 Meter -->0.772456411388215 Millimeter (Check conversion ​here)
FINAL ANSWER
0.772456411388215 0.772456 Millimeter <-- Required Thickness of Jacket
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Heet
Thadomal Shahani Engineering College (Tsec), Mumbai
Heet has created this Calculator and 200+ more calculators!
Verifier Image
Verified by Prerana Bakli
University of Hawaiʻi at Mānoa (UH Manoa), Hawaii, USA
Prerana Bakli has verified this Calculator and 1600+ more calculators!

21 Jacketed Reaction Vessel Calculators

Total Axial Stress in Vessel Shell
​ Go Total Axial Stress = ((Internal Pressure in Vessel*Internal Diameter of Shell)/(4*Shell Thickness*Joint Efficiency for Shell))+((Design Jacket Pressure*Internal Diameter of Half Coil)/(2*Shell Thickness*Joint Efficiency for Shell))+(2*Maximum difference between Coil and Shell Pressure*(Outer Diameter of Half Coil)^(2))/(3*Shell Thickness^(2))
Maximum Equivalent Stress at Junction with Shell
​ Go Maximum Equivalent Stress at Junction with Shell = (sqrt((Total Axial Stress)^(2)+(Total Hoop Stress)^(2)+(Maximum Hoop Stress in Coil at Junction with Shell)^(2)-((Total Axial Stress*Total Hoop Stress)+(Total Axial Stress*Maximum Hoop Stress in Coil at Junction with Shell)+(Maximum Hoop Stress in Coil at Junction with Shell*Total Hoop Stress))))
Total Hoop Stress in Shell
​ Go Total Hoop Stress = (Design Pressure Shell*Internal Diameter of Shell)/(2*Shell Thickness*Joint Efficiency for Shell)+(Design Jacket Pressure*Internal Diameter of Half Coil)/((4*Thickness of Half Coil Jacket*Weld Joint Efficiency Factor for Coil)+(2.5*Shell Thickness*Joint Efficiency for Shell))
Combined Moment of Inertia of Shell and Stiffener per Unit Length
​ Go Combined Moment of Inertia of Shell and Stiffener = (Vessel Shell Outer Diameter^(2)*Effective Length Between Stiffeners*(Shell Thickness for Jackted Reaction Vessel+Cross Sectional Area of Stiffening Ring/Effective Length Between Stiffeners)*Allowable Stress for Jacket Material)/(12*Modulus of Elasticity Jacketed Reaction Vessel)
Shell Thickness for Critical External Pressure
​ Go Critical External Pressure = (2.42*Modulus of Elasticity Jacketed Reaction Vessel)/(1-(Poisson Ratio)^(2))^(3/4)*((Vessel Thickness/Vessel Shell Outer Diameter)^(5/2)/((Length of Shell/Vessel Shell Outer Diameter)-0.45*(Vessel Thickness/Vessel Shell Outer Diameter)^(1/2)))
Depth of Torisperical Head
​ Go Depth of Head = Crown Radius for Jacketed Reaction Vessel-sqrt((Crown Radius for Jacketed Reaction Vessel-Vessel Shell Outer Diameter/2)*(Crown Radius for Jacketed Reaction Vessel+Vessel Shell Outer Diameter/2-2*Knuckle Radius))
Design of Shell Thickness Subjected to Internal Pressure
​ Go Shell Thickness for Jackted Reaction Vessel = (Internal Pressure in Vessel*Internal Diameter of Shell)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell)-(Internal Pressure in Vessel))+Corrosion Allowance
Maximum Axial Stress in Coil at Junction with Shell
​ Go Maximum Axial Stress in Coil at Junction = (Design Jacket Pressure*Internal Diameter of Half Coil)/((4*Thickness of Half Coil Jacket*Weld Joint Efficiency Factor for Coil)+(2.5*Shell Thickness*Joint Efficiency for Shell))
Dished Head Thickness
​ Go Dished Head Thickness = ((Internal Pressure in Vessel*Crown Radius for Jacketed Reaction Vessel*Stress Intensification Factor)/(2*Allowable Stress for Jacket Material*Joint Efficiency for Shell))+Corrosion Allowance
Thickness of Bottom Head subjected to Pressure
​ Go Head Thickness = 4.4*Crown Radius for Jacketed Reaction Vessel*(3*(1-(Poisson Ratio)^(2)))^(1/4)*sqrt(Internal Pressure in Vessel/(2*Modulus of Elasticity Jacketed Reaction Vessel))
Thickness of Half Coil Jacket
​ Go Thickness of Half Coil Jacket = (Design Jacket Pressure*Internal Diameter of Half Coil)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell))+Corrosion Allowance
Thickness of Jacket Shell for Internal Pressure
​ Go Required Thickness of Jacket = (Design Jacket Pressure*Internal Diameter of Shell)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell)-Design Jacket Pressure)
Channel Jacket Thickness
​ Go Channel Wall Thickness = Design Length of Channel Section*(sqrt((0.12*Design Jacket Pressure)/(Allowable Stress for Jacket Material)))+Corrosion Allowance
Maximum Hoop Stress in Coil at Junction with Shell
​ Go Maximum Hoop Stress in Coil at Junction with Shell = (Design Jacket Pressure*Internal Diameter of Half Coil)/(2*Thickness of Half Coil Jacket*Weld Joint Efficiency Factor for Coil)
Vessel Wall Thickness for Channel Type Jacket
​ Go Vessel Thickness = Design Length of Channel Section*sqrt((0.167*Design Jacket Pressure)/(Allowable Stress for Jacket Material))+Corrosion Allowance
Required Plate Thickness for Dimple Jacket
​ Go Required Thickness of Dimple Jacket = Maximum Pitch between Steam Weld Centre Lines*sqrt(Design Jacket Pressure/(3*Allowable Stress for Jacket Material))
Required Thickness for Jacket Closer Member with Jacket Width
​ Go Required Thickness for Jacket Closer Member = 0.886*Jacket Width*sqrt(Design Jacket Pressure/Allowable Stress for Jacket Material)
Length of Shell under Combined Moment of Inertia
​ Go Length of Shell = 1.1*sqrt(Vessel Shell Outer Diameter*Vessel Thickness)
Cross Sectional Area of Stiffening Ring
​ Go Cross Sectional Area of Stiffening Ring = Width of Stiffener*Thickness of Stiffener
Length of Shell for Jacket
​ Go Length of Shell for Jacket = Length of Straight Side Jacket+1/3*Depth of Head
Jacket Width
​ Go Jacket Width = (Inside Diameter of Jacket-Outer Diameter of Vessel)/2

Thickness of Jacket Shell for Internal Pressure Formula

Required Thickness of Jacket = (Design Jacket Pressure*Internal Diameter of Shell)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell)-Design Jacket Pressure)
trj = (pj*Di)/((2*fj*J)-pj)

What is Design Thickness?

Design thickness is a term used in structural engineering to refer to the thickness of a structural element (such as a beam, column, or plate) that has been calculated or specified based on the design requirements of the structure. The design thickness is the thickness that has been calculated or specified based on the structural requirements of the beam and the strength and deformability of the soil or foundation on which the beam will be supported. The design thickness of a bottom plate is typically determined by a structural engineer or using structural engineering software, and is used to ensure that the bottom plate is able to safely carry the loads that will be applied to it during the life of the structure.

How to Calculate Thickness of Jacket Shell for Internal Pressure?

Thickness of Jacket Shell for Internal Pressure calculator uses Required Thickness of Jacket = (Design Jacket Pressure*Internal Diameter of Shell)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell)-Design Jacket Pressure) to calculate the Required Thickness of Jacket, Thickness of Jacket Shell for Internal Pressure formula is defined as the distance from the external part to the internal part of a jacket shell. Required Thickness of Jacket is denoted by trj symbol.

How to calculate Thickness of Jacket Shell for Internal Pressure using this online calculator? To use this online calculator for Thickness of Jacket Shell for Internal Pressure, enter Design Jacket Pressure (pj), Internal Diameter of Shell (Di), Allowable Stress for Jacket Material (fj) & Joint Efficiency for Shell (J) and hit the calculate button. Here is how the Thickness of Jacket Shell for Internal Pressure calculation can be explained with given input values -> 772.4564 = (105000*1.5)/((2*120000000*0.85)-105000).

FAQ

What is Thickness of Jacket Shell for Internal Pressure?
Thickness of Jacket Shell for Internal Pressure formula is defined as the distance from the external part to the internal part of a jacket shell and is represented as trj = (pj*Di)/((2*fj*J)-pj) or Required Thickness of Jacket = (Design Jacket Pressure*Internal Diameter of Shell)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell)-Design Jacket Pressure). Design Jacket Pressure refers to a type of pressure vessel designed to withstand high pressures and temperatures, typically used for containing gases or liquids under extreme conditions, Internal Diameter of Shell is a measurement of the distance of a straight line from one point on the inner wall of the object, through its center, to an opposite point also on the inside, Allowable Stress for Jacket Material at Design Temperature is defined as the material failure stress divided by a factor of safety greater than one & Joint Efficiency for Shell refers to the effectiveness of the joint between two adjacent sections of a cylindrical shell, such as in a pressure vessel or a storage tank.
How to calculate Thickness of Jacket Shell for Internal Pressure?
Thickness of Jacket Shell for Internal Pressure formula is defined as the distance from the external part to the internal part of a jacket shell is calculated using Required Thickness of Jacket = (Design Jacket Pressure*Internal Diameter of Shell)/((2*Allowable Stress for Jacket Material*Joint Efficiency for Shell)-Design Jacket Pressure). To calculate Thickness of Jacket Shell for Internal Pressure, you need Design Jacket Pressure (pj), Internal Diameter of Shell (Di), Allowable Stress for Jacket Material (fj) & Joint Efficiency for Shell (J). With our tool, you need to enter the respective value for Design Jacket Pressure, Internal Diameter of Shell, Allowable Stress for Jacket Material & Joint Efficiency for Shell and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!