Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis Solution

STEP 0: Pre-Calculation Summary
Formula Used
Distance to 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)
ȳ = (𝜏*I*w)/(V*Aabove)
This formula uses 6 Variables
Variables Used
Distance to CG of Area from NA - (Measured in Meter) - Distance to CG of Area from NA is a distance helps in determining the distribution of stresses within a beam or any structural element.
Shear Stress at Section - (Measured in Pascal) - Shear stress at section is the internal force per unit area acting parallel to the cross-section of a material arises from shear forces, that act along the plane of the section.
Moment of Inertia of Area of Section - (Measured in Meter⁴) - Moment of inertia of area of section is a geometric property that measures how a cross-section’s area is distributed relative to an axis for predicting a beam’s resistance to bending and deflection.
Beam Width at Considered Level - (Measured in Meter) - Beam width at considered level is the width of a beam at a specific height or section along its length analyzed for the load distribution, shear forces, and bending moments within the beam.
Shear Force at Section - (Measured in Newton) - Shear force at section is the algebraic sum of all the vertical forces acting on one side of the section representing the internal force that acts parallel to the cross-section of the beam.
Area of Section above Considered Level - (Measured in Square Meter) - Area of section above considered level is the area of a section of a beam or other structural member that is above a certain reference level, used in calculations of shear stress and bending moments.
STEP 1: Convert Input(s) to Base Unit
Shear Stress at Section: 0.005 Megapascal --> 5000 Pascal (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)
Shear Force at Section: 4.9 Kilonewton --> 4900 Newton (Check conversion ​here)
Area of Section above Considered Level: 1986.063 Square Millimeter --> 0.001986063 Square Meter (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
ȳ = (𝜏*I*w)/(V*Aabove) --> (5000*0.00168*0.095)/(4900*0.001986063)
Evaluating ... ...
ȳ = 0.0819999883473701
STEP 3: Convert Result to Output's Unit
0.0819999883473701 Meter -->81.9999883473701 Millimeter (Check conversion ​here)
FINAL ANSWER
81.9999883473701 81.99999 Millimeter <-- Distance to CG of Area from NA
(Calculation completed in 00.020 seconds)

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National Institute Of Technology (NIT), Hamirpur
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Shear Stress at a Section Calculators

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

Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis Formula

​LaTeX ​Go
Distance to 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)
ȳ = (𝜏*I*w)/(V*Aabove)

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 Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis?

Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis calculator uses Distance to 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) to calculate the Distance to CG of Area from NA, Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis formula is defined as a measure of the vertical distance from the neutral axis to the centroid of the cross-sectional area above a considered level, used to calculate the shear stress at a section in a beam. Distance to CG of Area from NA is denoted by ȳ symbol.

How to calculate Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis using this online calculator? To use this online calculator for Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis, enter Shear Stress at Section (𝜏), Moment of Inertia of Area of Section (I), Beam Width at Considered Level (w), Shear Force at Section (V) & Area of Section above Considered Level (Aabove) and hit the calculate button. Here is how the Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis calculation can be explained with given input values -> 25446.43 = (5000*0.00168*0.095)/(4900*0.001986063).

FAQ

What is Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis?
Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis formula is defined as a measure of the vertical distance from the neutral axis to the centroid of the cross-sectional area above a considered level, used to calculate the shear stress at a section in a beam and is represented as ȳ = (𝜏*I*w)/(V*Aabove) or Distance to 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). Shear stress at section is the internal force per unit area acting parallel to the cross-section of a material arises from shear forces, that act along the plane of the section, Moment of inertia of area of section is a geometric property that measures how a cross-section’s area is distributed relative to an axis for predicting a beam’s resistance to bending and deflection, Beam width at considered level is the width of a beam at a specific height or section along its length analyzed for the load distribution, shear forces, and bending moments within the beam, Shear force at section is the algebraic sum of all the vertical forces acting on one side of the section representing the internal force that acts parallel to the cross-section of the beam & Area of section above considered level is the area of a section of a beam or other structural member that is above a certain reference level, used in calculations of shear stress and bending moments.
How to calculate Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis?
Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis formula is defined as a measure of the vertical distance from the neutral axis to the centroid of the cross-sectional area above a considered level, used to calculate the shear stress at a section in a beam is calculated using Distance to 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). To calculate Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis, you need Shear Stress at Section (𝜏), Moment of Inertia of Area of Section (I), Beam Width at Considered Level (w), Shear Force at Section (V) & Area of Section above Considered Level (Aabove). With our tool, you need to enter the respective value for 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 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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