Kethavath Srinath
Osmania University (OU), Hyderabad
Kethavath Srinath has created this Calculator and 50+ more calculators!
Alithea Fernandes
Don Bosco College of Engineering (DBCE), Goa
Alithea Fernandes has verified this Calculator and 50+ more calculators!

5 Other formulas that you can solve using the same Inputs

Critical Bending Coefficient
Bending Moment coefficient=(12.5*Maximum Moment)/((2.5*Maximum Moment)+(3*Moment at Quater point)+(4*Moment at Centerline)+(3*Moment at Three-quarter Point)) GO
Absolute Value of Moment at Three-Quarter Point of the Unbraced Beam Segment
Moment at Three-quarter Point=((12.5*Maximum Moment)-(2.5*Maximum Moment+4*Moment at Centerline+3*Moment at Quater point))/3 GO
Absolute Value of Moment at Quarter Point of the Unbraced Beam Segment
Moment at Quater point=((12.5*Maximum Moment)-(2.5*Maximum Moment+4*Moment at Centerline+3*Moment at Three-quarter Point))/3 GO
Absolute Value of Moment at Centerline of the Unbraced Beam Segment
Moment at Centerline=((12.5*Maximum Moment)-(2.5*Maximum Moment+3*Moment at Quater point+3*Moment at Three-quarter Point))/4 GO
Critical Bending Moment in Non-Uniform Bending
Non-Uniform Critical Bending Moment=(Bending Moment coefficient*Critical Bending Moment) GO

Absolute Value of Max Moment in the Unbraced Beam Segment Formula

Maximum Moment=(Bending Moment coefficient*((3*Moment at Quater point)+(4*Moment at Centerline)+(3*Moment at Three-quarter Point)))/(12.5-(Bending Moment coefficient*2.5))
More formulas
Bending Moment of Simply Supported Beams with Point Load at Centre GO
Bending Moment of Simply Supported Beams with Uniformly Distributed Load GO
Condition for Maximum Moment in Interior Spans of Beams GO
Greatest Safe Load for Solid Rectangle When Load in Middle GO
Greatest Safe Load for Solid Rectangle When Load is Distributed GO
Deflection for Solid Rectangle When Load in Middle GO
Deflection for Solid Rectangle When Load is Distributed GO
Greatest Safe Load for Hollow Rectangle When Load in Middle GO
Greatest Safe Load for Hollow Rectangle When Load is Distributed GO
Deflection for Hollow Rectangle When Load in Middle GO
Deflection for Hollow Rectangle When Load is Distributed GO
Greatest Safe Load for Solid Cylinder When Load in Middle GO
Greatest Safe Load for Solid Cylinder When Load is Distributed GO
Stress at Point y for a Curved Beam GO
Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam GO
Bending Moment When Stress is Applied at Point y in a Curved Beam GO
Critical Bending Moment in Non-Uniform Bending GO
Critical Bending Coefficient GO
Absolute Value of Moment at Quarter Point of the Unbraced Beam Segment GO
Absolute Value of Moment at Centerline of the Unbraced Beam Segment GO
Absolute Value of Moment at Three-Quarter Point of the Unbraced Beam Segment GO
Maximum Stress For Short Beams GO
Axial Load when Maximum Stress For Short Beams is Given GO
Cross-Sectional Area when Maximum Stress For Short Beams is Given GO
Maximum Bending Moment when Maximum Stress For Short Beams is Given GO
Total Unit Stress in Eccentric Loading GO
Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given GO
Neutral Axis to Outermost Fiber Distance when Total Unit Stress in Eccentric Loading is Given GO
Moment of Inertia of Cross-Section when Total Unit Stress in Eccentric Loading is Given GO
Total Unit Stress in Eccentric Loading when Radius of Gyration is Given GO
Eccentricity when Deflection in Eccentric Loading is Given GO
Bending Moment of Cantilever Beam subjected to Point Load at Free End GO
Bending Moment of a Cantilever Subject to UDL Over its Entire Span GO
Bending Moment Simply Supported Beam Subjected to a Concentrated Load GO
Bending Moment of Overhanging Beam Subjected to a Concentrated Load at Free End GO
Stress using Hook's Law GO
Fixed End Moment of a Fixed Beam having Point Load at Center GO
Fixed End Moment of a Fixed Beam having UDL over its entire Length GO
Fixed End Moment of a Fixed Beam carrying point load GO
Fixed End Moment of a Fixed Beam carrying Right Angled Triangular Load at Right Angled End A GO
Fixed End Moment of a Fixed Beam carrying Triangular Loading GO
Fixed End Moment of a Fixed Beam carrying two Equispaced Point Loads GO
Fixed End Moment of a Fixed Beam carrying three Equispaced Point Loads GO
Fixed End Moment of a Fixed Beam with Couple Moment GO
Maximum and Center Deflection of Simply Supported Beam carrying Point Load at Center GO
Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length GO
Maximum and Center Deflection of Cantilever Beam carrying Point Load at Free End GO
Maximum and Center Deflection of Cantilever Beam carrying Point Load at any point GO
Maximum and Center Deflection of Cantilever Beam with Couple Moment at Free End GO
Shear Load when Strain Energy in Shear is Given GO
Strain Energy in Shear GO
Length over which Deformation Takes Place when Strain Energy in Shear is Given GO
Shear Area when Strain Energy in Shear is Given GO
Shear Modulus of Elasticity when Strain Energy in Shear is Given GO
Strain Energy in Shear when Shear Deformation is Given GO
Strain Energy in Torsion GO
Torque when Strain Energy in Torsion is Given GO
Length over which Deformation Takes Place when Strain Energy in Torsion is Given GO
Polar Moment of Inertia when Strain Energy in Torsion is Given GO
Shear Modulus of Elasticity when Strain Energy in Torsion is Given GO
Strain Energy in Torsion when Angle of Twist is Given GO
Strain Energy in Bending GO
Bending Moment when Strain Energy in Bending is Given GO
Length over which Deformation Takes Place when Strain Energy in Bending is Given GO
Modulus of Elasticity when Strain Energy in Bending is Given GO
Moment of Inertia when Strain Energy in Bending is Given GO
Strain Energy in Bending when Angle Through which One Beam Rotates wrt Other End is Given GO

Define moment?

The Moment of a force is a measure of its tendency to cause a body to rotate about a specific point or axis. A moment is due to a force not having an equal and opposite force directly along its line of action.

How to Calculate Absolute Value of Max Moment in the Unbraced Beam Segment?

Absolute Value of Max Moment in the Unbraced Beam Segment calculator uses Maximum Moment=(Bending Moment coefficient*((3*Moment at Quater point)+(4*Moment at Centerline)+(3*Moment at Three-quarter Point)))/(12.5-(Bending Moment coefficient*2.5)) to calculate the Maximum Moment, The Absolute Value of Max Moment in the Unbraced Beam Segment formula is a measure of the bending effect that can occur when an external force (or moment) is applied to a structural element. . Maximum Moment and is denoted by Mmax symbol.

How to calculate Absolute Value of Max Moment in the Unbraced Beam Segment using this online calculator? To use this online calculator for Absolute Value of Max Moment in the Unbraced Beam Segment, enter Moment at Quater point (MA), Moment at Centerline (MB), Moment at Three-quarter Point (MC) and Bending Moment coefficient (Cb) and hit the calculate button. Here is how the Absolute Value of Max Moment in the Unbraced Beam Segment calculation can be explained with given input values -> -280 = (10*((3*30)+(4*50)+(3*20)))/(12.5-(10*2.5)).

FAQ

What is Absolute Value of Max Moment in the Unbraced Beam Segment?
The Absolute Value of Max Moment in the Unbraced Beam Segment formula is a measure of the bending effect that can occur when an external force (or moment) is applied to a structural element. and is represented as Mmax=(Cb*((3*MA)+(4*MB)+(3*MC)))/(12.5-(Cb*2.5)) or Maximum Moment=(Bending Moment coefficient*((3*Moment at Quater point)+(4*Moment at Centerline)+(3*Moment at Three-quarter Point)))/(12.5-(Bending Moment coefficient*2.5)). The moment at Quater point is the absolute value of the moment at the quarter point of the unbraced beam segment, The moment at Centerline is the absolute value of moment at the centerline of the unbraced beam segment, Moment at Three-quarter Point is the absolute value of moment at three-quarter point of the unbraced beam segment. and The Bending Moment coefficient of moments can be calculated by dividing the support moments by the span length.
How to calculate Absolute Value of Max Moment in the Unbraced Beam Segment?
The Absolute Value of Max Moment in the Unbraced Beam Segment formula is a measure of the bending effect that can occur when an external force (or moment) is applied to a structural element. is calculated using Maximum Moment=(Bending Moment coefficient*((3*Moment at Quater point)+(4*Moment at Centerline)+(3*Moment at Three-quarter Point)))/(12.5-(Bending Moment coefficient*2.5)). To calculate Absolute Value of Max Moment in the Unbraced Beam Segment, you need Moment at Quater point (MA), Moment at Centerline (MB), Moment at Three-quarter Point (MC) and Bending Moment coefficient (Cb). With our tool, you need to enter the respective value for Moment at Quater point, Moment at Centerline, Moment at Three-quarter Point and Bending Moment coefficient 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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