Alithea Fernandes
Don Bosco College of Engineering (DBCE), Goa
Alithea Fernandes has created this Calculator and 100+ more calculators!
Rudrani Tidke
Cummins College of Engineering for Women (CCEW), Pune
Rudrani Tidke has verified this Calculator and 50+ more calculators!

11 Other formulas that you can solve using the same Inputs

Surface Area of a Rectangular Prism
Surface Area=2*(Length*Width+Length*Height+Width*Height) GO
Perimeter of a rectangle when diagonal and length are given
Perimeter=2*(Length+sqrt((Diagonal)^2-(Length)^2)) GO
Magnetic Flux
Magnetic Flux=Magnetic Field*Length*Breadth*cos(θ) GO
Diagonal of a Rectangle when length and area are given
Diagonal=sqrt(((Area)^2/(Length)^2)+(Length)^2) GO
Area of a Rectangle when length and diagonal are given
Area=Length*(sqrt((Diagonal)^2-(Length)^2)) GO
Diagonal of a Rectangle when length and breadth are given
Diagonal=sqrt(Length^2+Breadth^2) GO
Strain
Strain=Change In Length/Length GO
Surface Tension
Surface Tension=Force/Length GO
Perimeter of a rectangle when length and width are given
Perimeter=2*Length+2*Width GO
Volume of a Rectangular Prism
Volume=Width*Height*Length GO
Area of a Rectangle when length and breadth are given
Area=Length*Breadth GO

Condition for Maximum Moment in Interior Spans of Beams Formula

Point of Maximum Moment=(Length/2)-(Maximum Bending Moment/(Uniformly Distributed Load*1000*Length))
x=(l/2)-(M/(q*1000*l))
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
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 Max Moment in the Unbraced Beam Segment 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

What is Condition for Maximum Moment in Interior Spans of Beams?

Bending Moment refers to the bending of the beam or any structure upon the action of the arbitrary load. Maximum bending moment in the beam occurs at the point of maximum stress. Also, maximum bending moment will be at the point where shear force changes its sign i.e., zero.

How to Calculate Condition for Maximum Moment in Interior Spans of Beams?

Condition for Maximum Moment in Interior Spans of Beams calculator uses Point of Maximum Moment=(Length/2)-(Maximum Bending Moment/(Uniformly Distributed Load*1000*Length)) to calculate the Point of Maximum Moment, The Condition for Maximum Moment in Interior Spans of Beams formula is defined as the distance from the support where the bending moment of a beam carrying uniformly distributed load is maximum and where the shear force is zero. Point of Maximum Moment and is denoted by x symbol.

How to calculate Condition for Maximum Moment in Interior Spans of Beams using this online calculator? To use this online calculator for Condition for Maximum Moment in Interior Spans of Beams, enter Length (l), Maximum Bending Moment (M) and Uniformly Distributed Load (q) and hit the calculate button. Here is how the Condition for Maximum Moment in Interior Spans of Beams calculation can be explained with given input values -> 1.5 = (3/2)-(10/(10000*1000*3)).

FAQ

What is Condition for Maximum Moment in Interior Spans of Beams?
The Condition for Maximum Moment in Interior Spans of Beams formula is defined as the distance from the support where the bending moment of a beam carrying uniformly distributed load is maximum and where the shear force is zero and is represented as x=(l/2)-(M/(q*1000*l)) or Point of Maximum Moment=(Length/2)-(Maximum Bending Moment/(Uniformly Distributed Load*1000*Length)). Length is the measurement or extent of something from end to end, The Maximum Bending Moment is the absolute value of the maximum moment in the unbraced beam segment and Uniformly distributed load is a force applied over an area or length, denoted by q which is force per unit length.
How to calculate Condition for Maximum Moment in Interior Spans of Beams?
The Condition for Maximum Moment in Interior Spans of Beams formula is defined as the distance from the support where the bending moment of a beam carrying uniformly distributed load is maximum and where the shear force is zero is calculated using Point of Maximum Moment=(Length/2)-(Maximum Bending Moment/(Uniformly Distributed Load*1000*Length)). To calculate Condition for Maximum Moment in Interior Spans of Beams, you need Length (l), Maximum Bending Moment (M) and Uniformly Distributed Load (q). With our tool, you need to enter the respective value for Length, Maximum Bending Moment and Uniformly Distributed Load and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Share Image
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!