Alithea Fernandes
Don Bosco College of Engineering (DBCE), Goa
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Rudrani Tidke
Cummins College of Engineering for Women (CCEW), Pune
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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

9 Other formulas that calculate the same Output

The Deflection at the Top Due to Uniform Load
Deflection=(1.5*Uniform Lateral Load*Height of the wall/(Modulus Of Elasticity*Wall thickness))*((Height of the wall/Length of wall)^3+(Height of the wall/Length of wall)) GO
The Deflection at the Top Due to Concentrated Load
Deflection=(4*Concentrated load/(Modulus Of Elasticity*Wall thickness))*((Height of the wall/Length of wall)^3+0.75*(Height of the wall/Length of wall)) GO
The Deflection at the Top Due to Fixed Against Rotation
Deflection=(Concentrated load/(Modulus Of Elasticity*Wall thickness))*((Height of the wall/Length of wall)^3+3*(Height of the wall/Length of wall)) GO
Maximum and Center Deflection of Cantilever Beam carrying Point Load at any point
Deflection=(Point Load acting on the Beam*(Distance from end A^2)*(3*Length-Distance from end A))/(6*Modulus Of Elasticity*Area Moment of Inertia) GO
Maximum and Center Deflection of Simply Supported Beam carrying Point Load at Center
Deflection=(Point Load acting on the Beam*(Length^3))/(48*Modulus Of Elasticity*Area Moment of Inertia) GO
Maximum and Center Deflection of Cantilever Beam carrying Point Load at Free End
Deflection=(Point Load acting on the Beam*(Length^3))/(3*Modulus Of Elasticity*Area Moment of Inertia) GO
Maximum and Center Deflection of Cantilever Beam with Couple Moment at Free End
Deflection=(Couple Moment*(Length^2))/(2*Modulus Of Elasticity*Area Moment of Inertia) GO
Deflection of fixed beam with load at center
Deflection=-Width*(Length^3)/(192*Elastic Modulus*Moment of Inertia) GO
Deflection of fixed beam with uniformly distributed load
Deflection=-Width*Length^4/(384*Elastic Modulus*Moment of Inertia) GO

Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length Formula

Deflection=(5*Uniformly Distributed Load*(Length^4))/(384*Modulus Of Elasticity*Area Moment of Inertia)
𝜕 =(5*q*(l^4))/(384*E*I)
More formulas
Maximum and Center Deflection of Simply Supported Beam carrying Point Load at Center 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

Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length

Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length is the degree to which a structural element is displaced under a load

How to Calculate Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length?

Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length calculator uses Deflection=(5*Uniformly Distributed Load*(Length^4))/(384*Modulus Of Elasticity*Area Moment of Inertia) to calculate the Deflection, The Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length formula is defined as (5*Uniformly Distributed Load*(length of Beam^4))/(384*Modulus of Elasticity*Area Moment of Inertia). Deflection and is denoted by 𝜕 symbol.

How to calculate Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length using this online calculator? To use this online calculator for Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length, enter Uniformly Distributed Load (q), Length (l), Modulus Of Elasticity (E) and Area Moment of Inertia (I) and hit the calculate button. Here is how the Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length calculation can be explained with given input values -> 0.010547 = (5*10000*(3^4))/(384*10000*100).

FAQ

What is Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length?
The Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length formula is defined as (5*Uniformly Distributed Load*(length of Beam^4))/(384*Modulus of Elasticity*Area Moment of Inertia) and is represented as 𝜕 =(5*q*(l^4))/(384*E*I) or Deflection=(5*Uniformly Distributed Load*(Length^4))/(384*Modulus Of Elasticity*Area Moment of Inertia). Uniformly distributed load is a force applied over an area or length, denoted by q which is force per unit length, Length is the measurement or extent of something from end to end, Modulus Of Elasticity is a quantity that measures an object or substance's resistance to being deformed elastically when a stress is applied to it and Area moment of inertia is a property of a two-dimensional plane shape which characterizes its deflection under loading.
How to calculate Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length?
The Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length formula is defined as (5*Uniformly Distributed Load*(length of Beam^4))/(384*Modulus of Elasticity*Area Moment of Inertia) is calculated using Deflection=(5*Uniformly Distributed Load*(Length^4))/(384*Modulus Of Elasticity*Area Moment of Inertia). To calculate Maximum and Center Deflection of Simply Supported Beam carrying UDL over its entire Length, you need Uniformly Distributed Load (q), Length (l), Modulus Of Elasticity (E) and Area Moment of Inertia (I). With our tool, you need to enter the respective value for Uniformly Distributed Load, Length, Modulus Of Elasticity and Area Moment of Inertia and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Deflection?
In this formula, Deflection uses Uniformly Distributed Load, Length, Modulus Of Elasticity and Area Moment of Inertia. We can use 9 other way(s) to calculate the same, which is/are as follows -
  • Deflection=-Width*(Length^3)/(192*Elastic Modulus*Moment of Inertia)
  • Deflection=-Width*Length^4/(384*Elastic Modulus*Moment of Inertia)
  • Deflection=(Point Load acting on the Beam*(Length^3))/(48*Modulus Of Elasticity*Area Moment of Inertia)
  • Deflection=(Point Load acting on the Beam*(Length^3))/(3*Modulus Of Elasticity*Area Moment of Inertia)
  • Deflection=(Point Load acting on the Beam*(Distance from end A^2)*(3*Length-Distance from end A))/(6*Modulus Of Elasticity*Area Moment of Inertia)
  • Deflection=(Couple Moment*(Length^2))/(2*Modulus Of Elasticity*Area Moment of Inertia)
  • Deflection=(1.5*Uniform Lateral Load*Height of the wall/(Modulus Of Elasticity*Wall thickness))*((Height of the wall/Length of wall)^3+(Height of the wall/Length of wall))
  • Deflection=(4*Concentrated load/(Modulus Of Elasticity*Wall thickness))*((Height of the wall/Length of wall)^3+0.75*(Height of the wall/Length of wall))
  • Deflection=(Concentrated load/(Modulus Of Elasticity*Wall thickness))*((Height of the wall/Length of wall)^3+3*(Height of the wall/Length of wall))
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