Area of Flange or Area above Considered Section Solution

STEP 0: Pre-Calculation Summary
Formula Used
Area of Section above Considered Level = Width of Beam Section*(Outer Depth of I section/2-Distance from Neutral Axis)
Aabv = B*(D/2-y)
This formula uses 4 Variables
Variables Used
Area of Section above Considered Level - (Measured in Square Meter) - Area of Section above Considered Level is the geometric area of a section of a system (such as a tank, basin, or duct) above a specific level. This level is often a reference point for analysis.
Width of Beam Section - (Measured in Meter) - Width of Beam Section is the width of the rectangular cross-section of the beam parallel to the axis in consideration.
Outer Depth of I section - (Measured in Meter) - The Outer Depth of I section is a measure of distance, the distance between the outer bars of the I-section.
Distance from Neutral Axis - (Measured in Meter) - Distance from Neutral Axis is the distance of the considered layer from the neutral layer.
STEP 1: Convert Input(s) to Base Unit
Width of Beam Section: 100 Millimeter --> 0.1 Meter (Check conversion ​here)
Outer Depth of I section: 9000 Millimeter --> 9 Meter (Check conversion ​here)
Distance from Neutral Axis: 5 Millimeter --> 0.005 Meter (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Aabv = B*(D/2-y) --> 0.1*(9/2-0.005)
Evaluating ... ...
Aabv = 0.4495
STEP 3: Convert Result to Output's Unit
0.4495 Square Meter -->449500 Square Millimeter (Check conversion ​here)
FINAL ANSWER
449500 Square Millimeter <-- Area of Section above Considered Level
(Calculation completed in 00.020 seconds)

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National Institute Of Technology (NIT), Hamirpur
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Shear Stress Distribution in Flange Calculators

Inner Depth of I-section given Shear Stress in Lower Edge of Flange
​ LaTeX ​ Go Inner Depth of I Section = sqrt(Outer Depth of I section^2-(8*Moment of Inertia of Area of Section)/Shear Force on Beam*Shear Stress in Beam)
Outer Depth of I section given Shear Stress in Lower Edge of Flange
​ LaTeX ​ Go Outer Depth of I section = sqrt((8*Moment of Inertia of Area of Section)/Shear Force on Beam*Shear Stress in Beam+Inner Depth of I Section^2)
Moment of Inertia of I section given Shear Stress in Lower Edge of Flange
​ LaTeX ​ Go Moment of Inertia of Area of Section = Shear Force on Beam/(8*Shear Stress in Beam)*(Outer Depth of I section^2-Inner Depth of I Section^2)
Shear Force in Lower Edge of Flange in I-section
​ LaTeX ​ Go Shear Force on Beam = (8*Moment of Inertia of Area of Section*Shear Stress in Beam)/(Outer Depth of I section^2-Inner Depth of I Section^2)

Area of Flange or Area above Considered Section Formula

​LaTeX ​Go
Area of Section above Considered Level = Width of Beam Section*(Outer Depth of I section/2-Distance from Neutral Axis)
Aabv = B*(D/2-y)

Where is Shear Stress Distribution in a Beam Section is Maximum?

In a rectangular beam:

Maximum shear stress occurs at the neutral axis (the horizontal axis through the centroid of the cross-section), which is typically at the mid-height of the beam.
Zero shear stress occurs at the outermost fibers (the top and bottom edges) of the beam's cross-section.
This means the shear stress is highest in the middle of the cross-section and decreases to zero as you move toward the top and bottom surfaces.

How to Calculate Area of Flange or Area above Considered Section?

Area of Flange or Area above Considered Section calculator uses Area of Section above Considered Level = Width of Beam Section*(Outer Depth of I section/2-Distance from Neutral Axis) to calculate the Area of Section above Considered Level, The Area of Flange or Area above Considered Section formula is defined as a measure of the cross-sectional area above the considered section in an I-shaped beam, which is essential in calculating the shear stress and other structural properties of the beam. Area of Section above Considered Level is denoted by Aabv symbol.

How to calculate Area of Flange or Area above Considered Section using this online calculator? To use this online calculator for Area of Flange or Area above Considered Section, enter Width of Beam Section (B), Outer Depth of I section (D) & Distance from Neutral Axis (y) and hit the calculate button. Here is how the Area of Flange or Area above Considered Section calculation can be explained with given input values -> 4.5E+11 = 0.1*(9/2-0.005).

FAQ

What is Area of Flange or Area above Considered Section?
The Area of Flange or Area above Considered Section formula is defined as a measure of the cross-sectional area above the considered section in an I-shaped beam, which is essential in calculating the shear stress and other structural properties of the beam and is represented as Aabv = B*(D/2-y) or Area of Section above Considered Level = Width of Beam Section*(Outer Depth of I section/2-Distance from Neutral Axis). Width of Beam Section is the width of the rectangular cross-section of the beam parallel to the axis in consideration, The Outer Depth of I section is a measure of distance, the distance between the outer bars of the I-section & Distance from Neutral Axis is the distance of the considered layer from the neutral layer.
How to calculate Area of Flange or Area above Considered Section?
The Area of Flange or Area above Considered Section formula is defined as a measure of the cross-sectional area above the considered section in an I-shaped beam, which is essential in calculating the shear stress and other structural properties of the beam is calculated using Area of Section above Considered Level = Width of Beam Section*(Outer Depth of I section/2-Distance from Neutral Axis). To calculate Area of Flange or Area above Considered Section, you need Width of Beam Section (B), Outer Depth of I section (D) & Distance from Neutral Axis (y). With our tool, you need to enter the respective value for Width of Beam Section, Outer Depth of I section & Distance from Neutral Axis 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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