Nominal tensile stress at edge of crack given load, plate thickness and plate width Calculator

✖Load on cracked plate is basically the amount of load/force that is acting on a cracked plate.ⓘ Load on cracked plate [L]			+10% -10%
✖Width of Plate is the width or the lateral dimension of the plate or a metal sheet under consideration.ⓘ Width of Plate [w]			+10% -10%
✖Thickness of Cracked Plate is the thickness or the minimum dimension of the plate or a metal sheet under consideration.ⓘ Thickness of Cracked Plate [t]			+10% -10%

✖Tensile Stress at Crack Edge is the amount of tensile stress at the edge of the crack of a structural member.ⓘ Nominal tensile stress at edge of crack given load, plate thickness and plate width [σ]

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Formula

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Nominal tensile stress at edge of crack given load, plate thickness and plate width

Formula

`"σ" = "L"/("w"*"t")`

Example

`"50N/mm²"="5250N"/("70mm"*"1.5mm")`

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Nominal tensile stress at edge of crack given load, plate thickness and plate width Solution

STEP 0: Pre-Calculation Summary

Formula Used

Tensile Stress at Crack Edge = Load on cracked plate/(Width of Plate*Thickness of Cracked Plate)
σ = L/(w*t)
This formula uses 4 Variables

Variables Used

Tensile Stress at Crack Edge - (Measured in Pascal) - Tensile Stress at Crack Edge is the amount of tensile stress at the edge of the crack of a structural member.
Load on cracked plate - (Measured in Newton) - Load on cracked plate is basically the amount of load/force that is acting on a cracked plate.
Width of Plate - (Measured in Meter) - Width of Plate is the width or the lateral dimension of the plate or a metal sheet under consideration.
Thickness of Cracked Plate - (Measured in Meter) - Thickness of Cracked Plate is the thickness or the minimum dimension of the plate or a metal sheet under consideration.

STEP 1: Convert Input(s) to Base Unit

Load on cracked plate: 5250 Newton --> 5250 Newton No Conversion Required
Width of Plate: 70 Millimeter --> 0.07 Meter (Check conversion here)
Thickness of Cracked Plate: 1.5 Millimeter --> 0.0015 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

σ = L/(w*t) --> 5250/(0.07*0.0015)

Evaluating ... ...

σ = 50000000

STEP 3: Convert Result to Output's Unit

50000000 Pascal -->50 Newton per Square Millimeter (Check conversion here)

FINAL ANSWER

50 Newton per Square Millimeter <-- Tensile Stress at Crack Edge

(Calculation completed in 00.004 seconds)

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< 10+ Fracture Mechanics Calculators

Fracture toughness given tensile stress at edge of crack

Go Fracture Toughness = Dimensionless Parameter in Fracture Toughness*(Tensile Stress at Crack Edge*(sqrt(pi*Half Crack Length)))

Nominal tensile stress at edge of crack given fracture toughness

Go Tensile Stress at Crack Edge = (Fracture Toughness/Dimensionless Parameter in Fracture Toughness)/sqrt(pi*Half Crack Length)

Half crack length given fracture toughness

Go Half Crack Length = (((Fracture Toughness/Dimensionless Parameter in Fracture Toughness)/(Tensile Stress at Crack Edge))^2)/pi

Nominal tensile stress at edge of crack given stress intensity factor

Go Tensile Stress at Crack Edge = (Stress Intensity Factor)/sqrt(pi*Half Crack Length)

Stress Intensity factor for cracked plate

Go Stress Intensity Factor = Tensile Stress at Crack Edge*(sqrt(pi*Half Crack Length))

Thickness of plate given nominal tensile stress at edge of crack

Go Thickness of Cracked Plate = Load on cracked plate/((Tensile Stress at Crack Edge)*(Width of Plate))

Width of plate given nominal tensile stress at edge of crack

Go Width of Plate = (Load on cracked plate/((Tensile Stress at Crack Edge)*Thickness of Cracked Plate))

Nominal tensile stress at edge of crack given load, plate thickness and plate width

Go Tensile Stress at Crack Edge = Load on cracked plate/(Width of Plate*Thickness of Cracked Plate)

Half crack length given stress intensity factor

Go Half Crack Length = ((Stress Intensity Factor/Tensile Stress at Crack Edge)^2)/pi

Fracture toughness given stress intensity factor

Go Fracture Toughness = Dimensionless Parameter in Fracture Toughness*Stress Intensity Factor

Nominal tensile stress at edge of crack given load, plate thickness and plate width Formula

Tensile Stress at Crack Edge = Load on cracked plate/(Width of Plate*Thickness of Cracked Plate)
σ = L/(w*t)

Beam vs Column

The beam is a horizontal structural component that mainly carries vertical loads. In contrast, columns are vertical compression members that span from substructure to superstructure and have a vital role in transferring load from the top of the structure to the foundation.

How to Calculate Nominal tensile stress at edge of crack given load, plate thickness and plate width?

Nominal tensile stress at edge of crack given load, plate thickness and plate width calculator uses Tensile Stress at Crack Edge = Load on cracked plate/(Width of Plate*Thickness of Cracked Plate) to calculate the Tensile Stress at Crack Edge, Nominal tensile stress at edge of crack given load, plate thickness and plate width is the amount of tensile stress at the edge of the crack of a plate. Tensile Stress at Crack Edge is denoted by σ symbol.

How to calculate Nominal tensile stress at edge of crack given load, plate thickness and plate width using this online calculator? To use this online calculator for Nominal tensile stress at edge of crack given load, plate thickness and plate width, enter Load on cracked plate (L), Width of Plate (w) & Thickness of Cracked Plate (t) and hit the calculate button. Here is how the Nominal tensile stress at edge of crack given load, plate thickness and plate width calculation can be explained with given input values -> 5E-5 = 5250/(0.07*0.0015).

FAQ

What is Nominal tensile stress at edge of crack given load, plate thickness and plate width?

Nominal tensile stress at edge of crack given load, plate thickness and plate width is the amount of tensile stress at the edge of the crack of a plate and is represented as σ = L/(w*t) or Tensile Stress at Crack Edge = Load on cracked plate/(Width of Plate*Thickness of Cracked Plate). Load on cracked plate is basically the amount of load/force that is acting on a cracked plate, Width of Plate is the width or the lateral dimension of the plate or a metal sheet under consideration & Thickness of Cracked Plate is the thickness or the minimum dimension of the plate or a metal sheet under consideration.

How to calculate Nominal tensile stress at edge of crack given load, plate thickness and plate width?

Nominal tensile stress at edge of crack given load, plate thickness and plate width is the amount of tensile stress at the edge of the crack of a plate is calculated using Tensile Stress at Crack Edge = Load on cracked plate/(Width of Plate*Thickness of Cracked Plate). To calculate Nominal tensile stress at edge of crack given load, plate thickness and plate width, you need Load on cracked plate (L), Width of Plate (w) & Thickness of Cracked Plate (t). With our tool, you need to enter the respective value for Load on cracked plate, Width of Plate & Thickness of Cracked Plate 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 Tensile Stress at Crack Edge?

In this formula, Tensile Stress at Crack Edge uses Load on cracked plate, Width of Plate & Thickness of Cracked Plate. We can use 2 other way(s) to calculate the same, which is/are as follows -

Tensile Stress at Crack Edge = (Stress Intensity Factor)/sqrt(pi*Half Crack Length)
Tensile Stress at Crack Edge = (Fracture Toughness/Dimensionless Parameter in Fracture Toughness)/sqrt(pi*Half Crack Length)

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