Shear Stress at Section Solution

STEP 0: Pre-Calculation Summary
Formula Used
Shear stress at section = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Moment of Inertia of Area of Section*Beam Width at Considered Level)
𝜏section = (S*Aabv*ȳ)/(I*w)
This formula uses 6 Variables
Variables Used
Shear stress at section - (Measured in Pascal) - Shear stress at section is a force tending to cause deformation of a material by slippage along a plane or planes parallel to the imposed stress.
Shear Force at Section - (Measured in Newton) - Shear Force at Section is the force that causes shear deformation to occur in the shear plane.
Area of Section above Considered Level - (Measured in Square Meter) - Area of Section above Considered Level can be defined as the space occupied by a flat shape or the surface of an object.
Distance of CG of Area from NA - (Measured in Meter) - Distance of CG of area from NA is a numerical measurement of how far apart objects or points are.
Moment of Inertia of Area of Section - (Measured in Meter⁴) - Moment of Inertia of Area of Section is the second moment of the area of the section about the neutral axis.
Beam Width at Considered Level - (Measured in Meter) - Beam Width at Considered Level is the description of how wide the beam is at that level.
STEP 1: Convert Input(s) to Base Unit
Shear Force at Section: 4.9 Kilonewton --> 4900 Newton (Check conversion ​here)
Area of Section above Considered Level: 6400 Square Millimeter --> 0.0064 Square Meter (Check conversion ​here)
Distance of CG of Area from NA: 82 Millimeter --> 0.082 Meter (Check conversion ​here)
Moment of Inertia of Area of Section: 0.00168 Meter⁴ --> 0.00168 Meter⁴ No Conversion Required
Beam Width at Considered Level: 95 Millimeter --> 0.095 Meter (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
𝜏section = (S*Aabv*ȳ)/(I*w) --> (4900*0.0064*0.082)/(0.00168*0.095)
Evaluating ... ...
𝜏section = 16112.2807017544
STEP 3: Convert Result to Output's Unit
16112.2807017544 Pascal -->0.0161122807017544 Megapascal (Check conversion ​here)
FINAL ANSWER
0.0161122807017544 0.016112 Megapascal <-- Shear stress at section
(Calculation completed in 00.004 seconds)

Credits

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Created by Anshika Arya
National Institute Of Technology (NIT), Hamirpur
Anshika Arya has created this Calculator and 2000+ more calculators!
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Verified by Dipto Mandal
Indian Institute of Information Technology (IIIT), Guwahati
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7 Shear Stress at a Section Calculators

Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis
​ Go Distance of CG of Area from NA = (Shear stress at section*Moment of Inertia of Area of Section*Beam Width at Considered Level)/(Shear Force at Section*Area of Section above Considered Level)
Moment of Inertia of Section about Neutral Axis
​ Go Moment of Inertia of Area of Section = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Shear stress at section*Beam Width at Considered Level)
Area of Section above Considered Level
​ Go Area of Section above Considered Level = (Shear stress at section*Moment of Inertia of Area of Section*Beam Width at Considered Level)/(Shear Force at Section*Distance of CG of Area from NA)
Width of Beam at Considered Level
​ Go Beam Width at Considered Level = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Moment of Inertia of Area of Section*Shear stress at section)
Shear Stress at Section
​ Go Shear stress at section = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Moment of Inertia of Area of Section*Beam Width at Considered Level)
Shear Force at Section
​ Go Shear Force at Section = (Shear stress at section*Moment of Inertia of Area of Section*Beam Width at Considered Level)/(Area of Section above Considered Level*Distance of CG of Area from NA)
Shear Force at Section given Shear Area
​ Go Shear Force at Section = Shear stress at section*Shear Area of beam

Shear Stress at Section Formula

Shear stress at section = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Moment of Inertia of Area of Section*Beam Width at Considered Level)
𝜏section = (S*Aabv*ȳ)/(I*w)

What is shear stress and strain?

Shear strain is the deformation of an object or medium under shear stress. The shear modulus is the elastic modulus in this case. Shear stress is caused by forces acting along the object's two parallel surfaces.

How to Calculate Shear Stress at Section?

Shear Stress at Section calculator uses Shear stress at section = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Moment of Inertia of Area of Section*Beam Width at Considered Level) to calculate the Shear stress at section, The Shear stress at section formula is defined as force tending to cause deformation of a material by slippage along a plane or planes parallel to the imposed stress. Shear stress at section is denoted by 𝜏section symbol.

How to calculate Shear Stress at Section using this online calculator? To use this online calculator for Shear Stress at Section, enter Shear Force at Section (S), Area of Section above Considered Level (Aabv), Distance of CG of Area from NA (ȳ), Moment of Inertia of Area of Section (I) & Beam Width at Considered Level (w) and hit the calculate button. Here is how the Shear Stress at Section calculation can be explained with given input values -> 4.9E-9 = (4900*0.0064*0.082)/(0.00168*0.095).

FAQ

What is Shear Stress at Section?
The Shear stress at section formula is defined as force tending to cause deformation of a material by slippage along a plane or planes parallel to the imposed stress and is represented as 𝜏section = (S*Aabv*ȳ)/(I*w) or Shear stress at section = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Moment of Inertia of Area of Section*Beam Width at Considered Level). Shear Force at Section is the force that causes shear deformation to occur in the shear plane, Area of Section above Considered Level can be defined as the space occupied by a flat shape or the surface of an object, Distance of CG of area from NA is a numerical measurement of how far apart objects or points are, Moment of Inertia of Area of Section is the second moment of the area of the section about the neutral axis & Beam Width at Considered Level is the description of how wide the beam is at that level.
How to calculate Shear Stress at Section?
The Shear stress at section formula is defined as force tending to cause deformation of a material by slippage along a plane or planes parallel to the imposed stress is calculated using Shear stress at section = (Shear Force at Section*Area of Section above Considered Level*Distance of CG of Area from NA)/(Moment of Inertia of Area of Section*Beam Width at Considered Level). To calculate Shear Stress at Section, you need Shear Force at Section (S), Area of Section above Considered Level (Aabv), Distance of CG of Area from NA (ȳ), Moment of Inertia of Area of Section (I) & Beam Width at Considered Level (w). With our tool, you need to enter the respective value for Shear Force at Section, Area of Section above Considered Level, Distance of CG of Area from NA, Moment of Inertia of Area of Section & Beam Width at Considered Level 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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