Cross-Sectional Area when Maximum Stress For Short Beams is Given Calculator

Category	Engineering ↺
Engineering	Civil ↺
Civil	Beams ↺
Beams	Combined Axial and Bending Loads ↺

✖Axial Load is defined as applying a force on a structure directly along an axis of the structureⓘ Axial Load [P]			+10% -10%
✖Maximum stress at crack tip due to the applied nominal stress.ⓘ Maximum stress at crack tip [σ_m]			+10% -10%
✖The Maximum Bending Moment is the absolute value of the maximum moment in the unbraced beam segment.ⓘ Maximum Bending Moment [M]			+10% -10%
✖The Distance from the Neutral axis is the distance from the neutral axis to any given fiber.ⓘ Distance from the Neutral axis [y]			+10% -10%
✖Moment of Inertia is the measure of the resistance of a body to angular acceleration about a given axis.ⓘ Moment of Inertia [I]			+10% -10%

✖Cross sectional area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specifies axis at a point.ⓘ Cross-Sectional Area when Maximum Stress For Short Beams is Given [A]

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Cross-Sectional Area when Maximum Stress For Short Beams is Given

Kethavath Srinath

Osmania University (OU), Hyderabad

Kethavath Srinath has created this Calculator and 400+ more calculators!

Alithea Fernandes

Don Bosco College of Engineering (DBCE), Goa

Alithea Fernandes has verified this Calculator and 100+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Maximum Stress For Short Beams

Maximum stress at crack tip=(Axial Load/Cross sectional area)+((Maximum Bending Moment*Distance from the Neutral axis)/Moment of Inertia) GO

Condition for Maximum Moment in Interior Spans of Beams

Point of Maximum Moment=(Length/2)-(Maximum Bending Moment/(Uniformly Distributed Load*1000*Length)) GO

Impulsive Torque

Impulsive Torque=(Moment of Inertia*(Final Angular Velocity-Angular velocity))/Time Taken to Travel GO

Strain Energy if moment value is given

Strain Energy=(Bending moment*Bending moment*Length)/(2*Elastic Modulus*Moment of Inertia) GO

Center of Gravity

Centre of gravity=Moment of Inertia/(Volume*(Centre of Buoyancy+Metacenter)) GO

Center of Buoyancy

Centre of Buoyancy=Moment of Inertia/(Volume*Centre of gravity)-Metacenter GO

Metacenter

Metacenter=Moment of Inertia/(Volume*Centre of gravity)-Centre of Buoyancy GO

Deflection of fixed beam with load at center

Deflection=-Width*(Length^3)/(192*Elastic Modulus*Moment of Inertia) GO

Section Modulus

Section Modulus=(Moment of Inertia)/(Distance from the Neutral axis) GO

Deflection of fixed beam with uniformly distributed load

Deflection=-Width*Length^4/(384*Elastic Modulus*Moment of Inertia) GO

Angular Momentum

Angular Momentum=Moment of Inertia*Angular Velocity GO

< 11 Other formulas that calculate the same Output

Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam

Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis)))) GO

Cross-Sectional Area when Axial Buckling Load for a Warped Section is Given

Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2))) GO

Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given

Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))) GO

Cross-sectional area of the rod if stress induced in rod due to impact load is known

Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2)) GO

Cross-Sectional Area when Elastic Critical Buckling Load is Given

Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus) GO

Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given

Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity) GO

Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given

Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant) GO

Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given

Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus) GO

Cross-sectional Area of Soil Conveying Flow when Rate of Flow of Water is Given

Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient)) GO

Total Cross-Sectional Area of Tensile Reinforcing

Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam) GO

Area when water flow equation is given

Cross sectional area=water flow/flow velocity GO

Cross-Sectional Area when Maximum Stress For Short Beams is Given Formula

Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia))
A=P/(σ<sub>m</sub>-(M*y/I))

More formulas

Maximum Stress For Short Beams GO

Axial Load when Maximum Stress For Short Beams is Given GO

Maximum Bending Moment when Maximum Stress For Short Beams is Given GO

Define Cross-sectional Area?

The cross-sectional area is the area of a two-dimensional shape that is obtained when a three-dimensional object - such as a cylinder - is sliced perpendicular to some specified axis at a point. For example, the cross-section of a cylinder - when sliced parallel to its base - is a circle.

How to Calculate Cross-Sectional Area when Maximum Stress For Short Beams is Given?

Cross-Sectional Area when Maximum Stress For Short Beams is Given calculator uses Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) to calculate the Cross sectional area, The Cross-Sectional Area when Maximum Stress For Short Beams is Given is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point. Cross sectional area and is denoted by A symbol.

How to calculate Cross-Sectional Area when Maximum Stress For Short Beams is Given using this online calculator? To use this online calculator for Cross-Sectional Area when Maximum Stress For Short Beams is Given, enter Axial Load (P), Maximum stress at crack tip (σ_m), Maximum Bending Moment (M), Distance from the Neutral axis (y) and Moment of Inertia (I) and hit the calculate button. Here is how the Cross-Sectional Area when Maximum Stress For Short Beams is Given calculation can be explained with given input values -> 1.634E-6 = 98.0664999999931/(60000000-(10*0.05/1.125)).

FAQ

What is Cross-Sectional Area when Maximum Stress For Short Beams is Given?

The Cross-Sectional Area when Maximum Stress For Short Beams is Given is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point and is represented as A=P/(σ_m-(M*y/I)) or Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)). Axial Load is defined as applying a force on a structure directly along an axis of the structure, Maximum stress at crack tip due to the applied nominal stress, The Maximum Bending Moment is the absolute value of the maximum moment in the unbraced beam segment, The Distance from the Neutral axis is the distance from the neutral axis to any given fiber and Moment of Inertia is the measure of the resistance of a body to angular acceleration about a given axis.

How to calculate Cross-Sectional Area when Maximum Stress For Short Beams is Given?

The Cross-Sectional Area when Maximum Stress For Short Beams is Given is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to some specified axis at a point is calculated using Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)). To calculate Cross-Sectional Area when Maximum Stress For Short Beams is Given, you need Axial Load (P), Maximum stress at crack tip (σ_m), Maximum Bending Moment (M), Distance from the Neutral axis (y) and Moment of Inertia (I). With our tool, you need to enter the respective value for Axial Load, Maximum stress at crack tip, Maximum Bending Moment, Distance from the Neutral axis and 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 Cross sectional area?

In this formula, Cross sectional area uses Axial Load, Maximum stress at crack tip, Maximum Bending Moment, Distance from the Neutral axis and Moment of Inertia. We can use 11 other way(s) to calculate the same, which is/are as follows -

Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis))))
Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis)))
Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus)
Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus)
Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant)
Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2)))
Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam)
Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity)
Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2))
Cross sectional area=water flow/flow velocity
Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient))

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