Cross Sectional Area of Stiffening Ring Calculator

✖Width of Stiffener in a vessel is the dimension of the stiffener measured perpendicular to its axis.ⓘ Width of Stiffener [W_s]			+10% -10%
✖Thickness of Stiffener in a vessel is the dimension of the stiffener measured perpendicular to its width and axis.ⓘ Thickness of Stiffener [T_s]			+10% -10%

✖Cross Sectional Area of Stiffening Ring in a vessel is the area of the ring when viewed in cross-section perpendicular to its axis.ⓘ Cross Sectional Area of Stiffening Ring [A_s]

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Formula

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Cross Sectional Area of Stiffening Ring

Formula

`"A"_{"s"} = "W"_{"s"}*"T"_{"s"}`

Example

`"1640mm²"="40mm"*"41mm"`

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Cross Sectional Area of Stiffening Ring Solution

STEP 0: Pre-Calculation Summary

Formula Used

Cross Sectional Area of Stiffening Ring = Width of Stiffener*Thickness of Stiffener
A_s = W_s*T_s
This formula uses 3 Variables

Variables Used

Cross Sectional Area of Stiffening Ring - (Measured in Square Millimeter) - Cross Sectional Area of Stiffening Ring in a vessel is the area of the ring when viewed in cross-section perpendicular to its axis.
Width of Stiffener - (Measured in Millimeter) - Width of Stiffener in a vessel is the dimension of the stiffener measured perpendicular to its axis.
Thickness of Stiffener - (Measured in Millimeter) - Thickness of Stiffener in a vessel is the dimension of the stiffener measured perpendicular to its width and axis.

STEP 1: Convert Input(s) to Base Unit

Width of Stiffener: 40 Millimeter --> 40 Millimeter No Conversion Required
Thickness of Stiffener: 41 Millimeter --> 41 Millimeter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

A_s = W_s*T_s --> 40*41

Evaluating ... ...

A_s = 1640

STEP 3: Convert Result to Output's Unit

0.00164 Square Meter -->1640 Square Millimeter (Check conversion here)

FINAL ANSWER

1640 Square Millimeter <-- Cross Sectional Area of Stiffening Ring

(Calculation completed in 00.004 seconds)

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< 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

Cross Sectional Area of Stiffening Ring Formula

Cross Sectional Area of Stiffening Ring = Width of Stiffener*Thickness of Stiffener
A_s = W_s*T_s

What is Jacketed Reaction Vessel?

A jacketed reaction vessel is a type of vessel used in the process of chemical reactions or mixing substances together under certain conditions. The vessel is typically made of a durable material such as stainless steel or glass and is designed to withstand high temperatures and pressures. The jacket surrounding the vessel is filled with a heating or cooling medium, such as water or oil, to control the temperature of the contents inside the vessel. The jacketed design allows for precise temperature control and uniform heating or cooling of the contents inside the vessel during the reaction process. These vessels are commonly used in chemical, pharmaceutical, and food processing industries.

What is Cross Sectional Area?

Cross-sectional area refers to the area of a two-dimensional shape when it is viewed from a cross-section perspective. In other words, it is the area of the shape that is exposed when it is cut through by a plane that is perpendicular to its base. In engineering and physics, cross-sectional area is often used to calculate properties such as force, pressure, and flow rate. For example, the cross-sectional area of a pipe is used to calculate the flow rate of fluid passing through it.

How to Calculate Cross Sectional Area of Stiffening Ring?

Cross Sectional Area of Stiffening Ring calculator uses Cross Sectional Area of Stiffening Ring = Width of Stiffener*Thickness of Stiffener to calculate the Cross Sectional Area of Stiffening Ring, The Cross Sectional Area of Stiffening Ring is a measure of the area of a two-dimensional shape that is perpendicular to an axis. In other words, it is the area of a shape when it is sliced perpendicular to its axis. Cross Sectional Area of Stiffening Ring is denoted by A_s symbol.

How to calculate Cross Sectional Area of Stiffening Ring using this online calculator? To use this online calculator for Cross Sectional Area of Stiffening Ring, enter Width of Stiffener (W_s) & Thickness of Stiffener (T_s) and hit the calculate button. Here is how the Cross Sectional Area of Stiffening Ring calculation can be explained with given input values -> 1.6E+9 = 0.04*0.041.

FAQ

What is Cross Sectional Area of Stiffening Ring?

The Cross Sectional Area of Stiffening Ring is a measure of the area of a two-dimensional shape that is perpendicular to an axis. In other words, it is the area of a shape when it is sliced perpendicular to its axis and is represented as A_s = W_s*T_s or Cross Sectional Area of Stiffening Ring = Width of Stiffener*Thickness of Stiffener. Width of Stiffener in a vessel is the dimension of the stiffener measured perpendicular to its axis & Thickness of Stiffener in a vessel is the dimension of the stiffener measured perpendicular to its width and axis.

How to calculate Cross Sectional Area of Stiffening Ring?

The Cross Sectional Area of Stiffening Ring is a measure of the area of a two-dimensional shape that is perpendicular to an axis. In other words, it is the area of a shape when it is sliced perpendicular to its axis is calculated using Cross Sectional Area of Stiffening Ring = Width of Stiffener*Thickness of Stiffener. To calculate Cross Sectional Area of Stiffening Ring, you need Width of Stiffener (W_s) & Thickness of Stiffener (T_s). With our tool, you need to enter the respective value for Width of Stiffener & Thickness of Stiffener 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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