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
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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 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/(σm-(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 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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