Shear Force in End Members at First Interior Support Calculator

Category	Engineering ↺
Engineering	Civil ↺
Civil	Concrete ↺
Concrete	Continuous Beams and One Way Slabs ↺

✖Force is the instantaneous load applied perpendicular to the specimen cross section.ⓘ Force [F]			+10% -10%
✖Length of Span refers to the length of the opening above which the beam is spanning.ⓘ Length of Span [I_n]			+10% -10%

✖moment is an overturning effect (tends to bend or turn the member) created by the force(load) acting on a structural member.ⓘ Shear Force in End Members at First Interior Support [M_t]

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Shear Force in End Members at First Interior Support

Kethavath Srinath

Osmania University (OU), Hyderabad

Kethavath Srinath has created this Calculator and 400+ 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

Brinell Hardness Number

Brinell Hardness Number=Force/((0.5*pi*Diameter of the ball indentor)*(Diameter of the ball indentor-((Diameter of the ball indentor^2)-(Diameter of indentation^2))^0.5)) GO

Deflection of the center of the leaf spring in pickering governor

Deflection of the centre of the leaf spring=(Force*Distance between the fixed ends of the spring^3)/(192*Young’s modulus of the material of the spring*Moment of Inertia) GO

Stress due to impact loading

Stress=Force*(1+sqrt(1+2*Original cross sectional area*Elastic Modulus*Height at which load falls/Force*Length))/Original cross sectional area GO

Elongation circular tapered bar

Elongation=4*Force*Length/(pi*Diameter of bigger end*Diameter of smaller end *Elastic Modulus) GO

Thermal Stress in tapered bar

Stress=(4*Force*Length)/(pi*Diameter of bigger end*Diameter of smaller end *Elastic Modulus) GO

Elongation of prismatic bar due to its own weight

Elongation=2*Force*Length of Rod/(Area*Elastic Modulus) GO

Engineering stress

Engineering stress=Force/Original cross sectional area GO

Hooke's law

Young's Modulus=Force*Elongation/(Area*Initial length) GO

Axial elongation of prismatic bar due to external load

Elongation=Force*Length of Rod/(Area*Elastic Modulus) GO

Strain Energy if applied tension load is given

Strain Energy=Force^2*Length/(2*Area*Young's Modulus) GO

Positive Moment for End Spans if Discontinuous End is Unrestrained

moment=(Force*Length of Span^2)/11 GO

< 9 Other formulas that calculate the same Output

Negative Moment at Interior Faces of Exterior Supports where Support is a Spandrel Beam

moment=(Force*Length of Span^2)/24 GO

Negative Moment at Exterior Face of First Interior Support for More Than Two Spans

moment=(Force*Length of Span^2)/10 GO

Negative Moment at Interior Faces of Exterior Support where Support is a Column

moment=(Force*Length of Span^2)/12 GO

Positive Moment for End Spans if Discontinuous End is Integral with Support

moment=(Force*Length of Span^2)/14 GO

Positive Moment for End Spans if Discontinuous End is Unrestrained

moment=(Force*Length of Span^2)/11 GO

Negative Moment at Other Faces of Interior Supports

moment=(Force*Length of Span^2)/11 GO

Positive Moment for Interior Spans

moment=(Force*Length of Span^2)/16 GO

Negative Moment at Exterior Face of First Interior Support for Two Spans

moment=(Force*Length of Span^2)/9 GO

Shear Force at All Other Supports

moment=(Force*Length of Span^2)/2 GO

Shear Force in End Members at First Interior Support Formula

moment=1.15*(Force*Length of Span^2)/2
M<sub>t</sub>=1.15*(F*I<sub>n^2)/2

More formulas

Positive Moment for End Spans if Discontinuous End is Unrestrained GO

Positive Moment for End Spans if Discontinuous End is Integral with Support GO

Positive Moment for Interior Spans GO

Negative Moment at Exterior Face of First Interior Support for Two Spans GO

Negative Moment at Exterior Face of First Interior Support for More Than Two Spans GO

Negative Moment at Other Faces of Interior Supports GO

Negative Moment at Interior Faces of Exterior Supports where Support is a Spandrel Beam GO

Negative Moment at Interior Faces of Exterior Support where Support is a Column GO

Shear Force at All Other Supports GO

Define Shear Force?

A shear force is a force applied perpendicular to a surface, in opposition to an offset force acting in the opposite direction. ... When a structural member experiences failure by shear, two parts of it are pushed in different directions, for example, when a piece of paper is cut by scissors.

How to Calculate Shear Force in End Members at First Interior Support?

Shear Force in End Members at First Interior Support calculator uses moment=1.15*(Force*Length of Span^2)/2 to calculate the moment, The Shear Force in End Members at First Interior Support formula is defined as the force applied perpendicular to a surface, in opposition to an offset force acting in the opposite direction. moment and is denoted by M_t symbol.

How to calculate Shear Force in End Members at First Interior Support using this online calculator? To use this online calculator for Shear Force in End Members at First Interior Support, enter Force (F) and Length of Span (I_n) and hit the calculate button. Here is how the Shear Force in End Members at First Interior Support calculation can be explained with given input values -> 0.0575 = 1.15*(1000*0.01^2)/2.

FAQ

What is Shear Force in End Members at First Interior Support?

The Shear Force in End Members at First Interior Support formula is defined as the force applied perpendicular to a surface, in opposition to an offset force acting in the opposite direction and is represented as M_t=1.15*(F*I_n^2)/2 or moment=1.15*(Force*Length of Span^2)/2. Force is the instantaneous load applied perpendicular to the specimen cross section and Length of Span refers to the length of the opening above which the beam is spanning.

How to calculate Shear Force in End Members at First Interior Support?

The Shear Force in End Members at First Interior Support formula is defined as the force applied perpendicular to a surface, in opposition to an offset force acting in the opposite direction is calculated using moment=1.15*(Force*Length of Span^2)/2. To calculate Shear Force in End Members at First Interior Support, you need Force (F) and Length of Span (I_n). With our tool, you need to enter the respective value for Force and Length of Span 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 moment?

In this formula, moment uses Force and Length of Span. We can use 9 other way(s) to calculate the same, which is/are as follows -

moment=(Force*Length of Span^2)/11
moment=(Force*Length of Span^2)/14
moment=(Force*Length of Span^2)/16
moment=(Force*Length of Span^2)/9
moment=(Force*Length of Span^2)/10
moment=(Force*Length of Span^2)/11
moment=(Force*Length of Span^2)/24
moment=(Force*Length of Span^2)/12
moment=(Force*Length of Span^2)/2

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