Shear Failure Load on plate Calculator

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✖Distance between rivet and edge of plate defines the length calculated from the center of the rivet to the edge of the plate.ⓘ Distance between Rivet and Edge of Plate [a]			+10% -10%
✖Plate Thickness is the distance through the bearing plate.ⓘ Plate Thickness [p_t]			+10% -10%
✖Maximum Shear Stress is the force acting that acting on a coplanar cross-section of material due to the effect of shear forces.ⓘ Maximum Shear Stress [𝜏_max]			+10% -10%
✖Distance between Rivets is the space between the two rivets present in a joint.ⓘ Distance between Rivets [b]			+10% -10%

✖Edge Load per unit width is the force acting on the edges of an object having a unit width.ⓘ Shear Failure Load on plate [P]

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Formula

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Shear Failure Load on plate

Formula

`"P" = (2*"a"*"p"_{"t"}*"𝜏"_{"max"})/("b")`

Example

`"35.11284N/mm"=(2*"4mm"*"94mm"*"60N/mm²")/("1285mm")`

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Shear Failure Load on plate Solution

STEP 0: Pre-Calculation Summary

Formula Used

Edge Load per Unit Width = (2*Distance between Rivet and Edge of Plate*Plate Thickness*Maximum Shear Stress)/(Distance between Rivets)
P = (2*a*p_t*𝜏_max)/(b)
This formula uses 5 Variables

Variables Used

Edge Load per Unit Width - (Measured in Newton per Meter) - Edge Load per unit width is the force acting on the edges of an object having a unit width.
Distance between Rivet and Edge of Plate - (Measured in Meter) - Distance between rivet and edge of plate defines the length calculated from the center of the rivet to the edge of the plate.
Plate Thickness - (Measured in Meter) - Plate Thickness is the distance through the bearing plate.
Maximum Shear Stress - (Measured in Pascal) - Maximum Shear Stress is the force acting that acting on a coplanar cross-section of material due to the effect of shear forces.
Distance between Rivets - (Measured in Meter) - Distance between Rivets is the space between the two rivets present in a joint.

STEP 1: Convert Input(s) to Base Unit

Distance between Rivet and Edge of Plate: 4 Millimeter --> 0.004 Meter (Check conversion here)
Plate Thickness: 94 Millimeter --> 0.094 Meter (Check conversion here)
Maximum Shear Stress: 60 Newton per Square Millimeter --> 60000000 Pascal (Check conversion here)
Distance between Rivets: 1285 Millimeter --> 1.285 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

P = (2*a*p_t*𝜏_max)/(b) --> (2*0.004*0.094*60000000)/(1.285)

Evaluating ... ...

P = 35112.8404669261

STEP 3: Convert Result to Output's Unit

35112.8404669261 Newton per Meter -->35.1128404669261 Newton per Millimeter (Check conversion here)

FINAL ANSWER

35.1128404669261 ≈ 35.11284 Newton per Millimeter <-- Edge Load per Unit Width

(Calculation completed in 00.004 seconds)

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Created by Shreyash

Rajiv Gandhi Institute of Technology (RGIT), Mumbai

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< 9 Structural Design Calculators

Ultimate Tensile Stress for Plate

Go Ultimate Tensile Strength = (Edge Load per Unit Width*Distance between Rivets)/(Plate Thickness*(Distance between Rivets-Diameter of Rivet))

Shear Failure Load on plate

Go Edge Load per Unit Width = (2*Distance between Rivet and Edge of Plate*Plate Thickness*Maximum Shear Stress)/(Distance between Rivets)

Maximum Blade Efficiency

Go Maximum Blade Efficiency = (2*Blade Lift Force/Blade Drag Force-1)/(2*Blade Lift Force/Blade Drag Force+1)

Allowable Bearing Pressure

Go Bearing Stress = (Edge Load per Unit Width*Distance between Rivets)/(Plate Thickness*Diameter of Rivet)

Shear Load per width

Go Edge Load per Unit Width = (pi*(Diameter^2)*Maximum Shear Stress)/(4*Distance between Rivets)

Joint Efficiency

Go Joint Efficiency for Shell = (Distance between Rivets-Diameter)/(Distance between Rivets)

Disk Loading

Go Load = Aircraft Weight/((pi*Diameter of Rotor^2)/4)

Average Blade Lift Coefficient

Go Blade Lift Coefficient = 6*Thrust Coefficient/Rotor Solidity

Life of Aircraft given number of Flight

Go Number of Flights = (1/Total Damage per Flight)

Shear Failure Load on plate Formula

Edge Load per Unit Width = (2*Distance between Rivet and Edge of Plate*Plate Thickness*Maximum Shear Stress)/(Distance between Rivets)
P = (2*a*p_t*𝜏_max)/(b)

Site of shear failure in a plane?

Shearing of the plates may occur on the planes cc resulting in the rivets being dragged out of the plate.

How to Calculate Shear Failure Load on plate?

Shear Failure Load on plate calculator uses Edge Load per Unit Width = (2*Distance between Rivet and Edge of Plate*Plate Thickness*Maximum Shear Stress)/(Distance between Rivets) to calculate the Edge Load per Unit Width, Shear Failure Load on plate refers to the maximum shear force that a plate can withstand before experiencing failure due to shear stress, it occurs when the applied shear force exceeds the material's shear strength, leading to deformation, rupture, or fracture along the plane of the force. Edge Load per Unit Width is denoted by P symbol.

How to calculate Shear Failure Load on plate using this online calculator? To use this online calculator for Shear Failure Load on plate, enter Distance between Rivet and Edge of Plate (a), Plate Thickness (p_t), Maximum Shear Stress (𝜏_max) & Distance between Rivets (b) and hit the calculate button. Here is how the Shear Failure Load on plate calculation can be explained with given input values -> 0.035698 = (2*0.004*0.094*60000000)/(1.285).

FAQ

What is Shear Failure Load on plate?

Shear Failure Load on plate refers to the maximum shear force that a plate can withstand before experiencing failure due to shear stress, it occurs when the applied shear force exceeds the material's shear strength, leading to deformation, rupture, or fracture along the plane of the force and is represented as P = (2*a*p_t*𝜏_max)/(b) or Edge Load per Unit Width = (2*Distance between Rivet and Edge of Plate*Plate Thickness*Maximum Shear Stress)/(Distance between Rivets). Distance between rivet and edge of plate defines the length calculated from the center of the rivet to the edge of the plate, Plate Thickness is the distance through the bearing plate, Maximum Shear Stress is the force acting that acting on a coplanar cross-section of material due to the effect of shear forces & Distance between Rivets is the space between the two rivets present in a joint.

How to calculate Shear Failure Load on plate?

Shear Failure Load on plate refers to the maximum shear force that a plate can withstand before experiencing failure due to shear stress, it occurs when the applied shear force exceeds the material's shear strength, leading to deformation, rupture, or fracture along the plane of the force is calculated using Edge Load per Unit Width = (2*Distance between Rivet and Edge of Plate*Plate Thickness*Maximum Shear Stress)/(Distance between Rivets). To calculate Shear Failure Load on plate, you need Distance between Rivet and Edge of Plate (a), Plate Thickness (p_t), Maximum Shear Stress (𝜏_max) & Distance between Rivets (b). With our tool, you need to enter the respective value for Distance between Rivet and Edge of Plate, Plate Thickness, Maximum Shear Stress & Distance between Rivets 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 Edge Load per Unit Width?

In this formula, Edge Load per Unit Width uses Distance between Rivet and Edge of Plate, Plate Thickness, Maximum Shear Stress & Distance between Rivets. We can use 1 other way(s) to calculate the same, which is/are as follows -

Edge Load per Unit Width = (pi*(Diameter^2)*Maximum Shear Stress)/(4*Distance between Rivets)

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