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 can be defined as the space occupied by a flat shape or the surface of an object.
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 00.004 seconds)

Credits

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

Distance of Considered Section from Neutral Axis given Shear Stress in Flange
Go Distance from Neutral Axis = sqrt((Outer Depth of I section^2)/2-(2*Moment of Inertia of Area of Section)/Shear Force on Beam*Shear Stress in Beam)
Outer Depth of I-section given Shear Stress in Flange
Go Outer Depth of I section = 4*sqrt((2*Moment of Inertia of Area of Section)/Shear Force on Beam*Shear Stress in Beam+Distance from Neutral Axis^2)
Inner Depth of I-section given Shear Stress in Lower Edge of Flange
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
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 Section for I-section
Go Moment of Inertia of Area of Section = Shear Force on Beam/(2*Shear Stress in Beam)*((Outer Depth of I section^2)/2-Distance from Neutral Axis^2)
Shear Force in Flange of I-section
Go Shear Force on Beam = (2*Moment of Inertia of Area of Section*Shear Stress in Beam)/((Outer Depth of I section^2)/2-Distance from Neutral Axis^2)
Shear Stress in Flange of I-section
Go Shear Stress in Beam = Shear Force on Beam/(2*Moment of Inertia of Area of Section)*(Outer Depth of I section^2/2-Distance from Neutral Axis^2)
Moment of Inertia of I section given Shear Stress in Lower Edge of Flange
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 Stress in Lower Edge of Flange of I-section
Go Shear Stress in Beam = Shear Force on Beam/(8*Moment of Inertia of Area of Section)*(Outer Depth of I section^2-Inner Depth of I Section^2)
Shear Force in Lower Edge of Flange in I-section
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)
Width of Section given Area above Considered Section of Flange
Go Width of Beam Section = Area of Section above Considered Level/(Outer Depth of I section/2-Distance from Neutral Axis)
Area of Flange or Area above Considered Section
Go Area of Section above Considered Level = Width of Beam Section*(Outer Depth of I section/2-Distance from Neutral Axis)
Distance of CG of Considered Area of Flange from Neutral Axis in I Section
Go Distance of CG of Area from NA = 1/2*(Outer Depth of I section/2+Distance from Neutral Axis)
Distance of Lower Edge of Flange from Neutral Axis
Go Distance from Neutral Axis = Inner Depth of I Section/2
Distance of Upper Edge of Flange from Neutral Axis
Go Distance from Neutral Axis = Outer Depth of I section/2

Area of Flange or Area above Considered Section Formula

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 maximum?

The maximum shear stress occurs at the neutral axis and is zero at both the top and bottom surface of the beam. Shear flow has the units of force per unit distance.

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 the space occupied by a flange. 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 the space occupied by a flange 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 the space occupied by a flange 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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