Thickness of plate given nominal tensile stress at edge of crack 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%
✖Tensile Stress at Crack Edge is the amount of tensile stress at the edge of the crack of a structural member.ⓘ Tensile Stress at Crack Edge [σ]			+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 plate given nominal tensile stress at edge of crack [t]

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Thickness of plate given nominal tensile stress at edge of crack Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

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.
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.
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.
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.

STEP 1: Convert Input(s) to Base Unit

Load on cracked plate: 5250 Newton --> 5250 Newton No Conversion Required
Tensile Stress at Crack Edge: 50 Newton per Square Millimeter --> 50000000 Pascal (Check conversion here)
Width of Plate: 70 Millimeter --> 0.07 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

t = L/((σ)*(w)) --> 5250/((50000000)*(0.07))

Evaluating ... ...

t = 0.0015

STEP 3: Convert Result to Output's Unit

0.0015 Meter -->1.5 Millimeter (Check conversion here)

FINAL ANSWER

1.5 Millimeter <-- Thickness of Cracked Plate

(Calculation completed in 00.004 seconds)

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< Fracture Mechanics Calculators

Nominal tensile stress at edge of crack given stress intensity factor

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

Stress Intensity factor for cracked plate

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

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

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

Half crack length given stress intensity factor

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

Thickness of plate given nominal tensile stress at edge of crack Formula

LaTeX Go

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

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 Thickness of plate given nominal tensile stress at edge of crack?

Thickness of plate given nominal tensile stress at edge of crack calculator uses Thickness of Cracked Plate = Load on cracked plate/((Tensile Stress at Crack Edge)*(Width of Plate)) to calculate the Thickness of Cracked Plate, Thickness of plate given nominal tensile stress at edge of crack is the thickness or the shortest dimension of a plate for which the stress near the crack is calculated. Thickness of Cracked Plate is denoted by t symbol.

How to calculate Thickness of plate given nominal tensile stress at edge of crack using this online calculator? To use this online calculator for Thickness of plate given nominal tensile stress at edge of crack, enter Load on cracked plate (L), Tensile Stress at Crack Edge (σ) & Width of Plate (w) and hit the calculate button. Here is how the Thickness of plate given nominal tensile stress at edge of crack calculation can be explained with given input values -> 1500 = 5250/((50000000)*(0.07)).

FAQ

What is Thickness of plate given nominal tensile stress at edge of crack?

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

How to calculate Thickness of plate given nominal tensile stress at edge of crack?

Thickness of plate given nominal tensile stress at edge of crack is the thickness or the shortest dimension of a plate for which the stress near the crack is calculated is calculated using Thickness of Cracked Plate = Load on cracked plate/((Tensile Stress at Crack Edge)*(Width of Plate)). To calculate Thickness of plate given nominal tensile stress at edge of crack, you need Load on cracked plate (L), Tensile Stress at Crack Edge (σ) & Width of Plate (w). With our tool, you need to enter the respective value for Load on cracked plate, Tensile Stress at Crack Edge & Width of Plate 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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