Kethavath Srinath
Osmania University (OU), Hyderabad
Kethavath Srinath has created this Calculator and 25+ more calculators!
Alithea Fernandes
Don Bosco College of Engineering (DBCE), Goa
Alithea Fernandes has verified this Calculator and 50+ more calculators!

11 Other formulas that you can solve using the same Inputs

Electric Current when Drift Velocity is Given
Electric Current=Number of free charge particles per unit volume*[Charge-e]*Cross sectional area*Drift Velocity 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
Resistance
Resistance=(Resistivity*Length of Conductor)/Cross sectional area GO
Angular Momentum
Angular Momentum=Moment of Inertia*Angular Velocity GO

Axial Load when Maximum Stress For Short Beams is Given Formula

Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia))
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
Condition for Maximum Moment in Interior Spans of Beams 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
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

Define axial Load?

An axial load is the compression or tension force acting in a member. If the axial load acts through the centroid of the member it is called concentric loading. If the force is not acting through the centroid it's called eccentric loading. Eccentric loading produces a moment in the beam as a result of the load being a distance away from the centroid.

How to Calculate Axial Load when Maximum Stress For Short Beams is Given?

Axial Load when Maximum Stress For Short Beams is Given calculator uses Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) to calculate the Axial Load, Axial Load when Maximum Stress For Short Beams is Given is defined as applying a force on a structure directly along an axis of the structure. Axial Load and is denoted by P symbol.

How to calculate Axial Load when Maximum Stress For Short Beams is Given using this online calculator? To use this online calculator for Axial Load when Maximum Stress For Short Beams is Given, enter Moment of Inertia (I), Cross sectional area (A), Maximum stress at crack tip m), Distance from the Neutral axis (y) and Maximum Bending Moment (M) and hit the calculate button. Here is how the Axial Load when Maximum Stress For Short Beams is Given calculation can be explained with given input values -> 6.118E+7 = 10*(60000000-(10*0.05/1.125)).

FAQ

What is Axial Load when Maximum Stress For Short Beams is Given?
Axial Load when Maximum Stress For Short Beams is Given is defined as applying a force on a structure directly along an axis of the structure and is represented as P=A*(σm-(M*y/I)) or Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)). Moment of Inertia is the measure of the resistance of a body to angular acceleration about a given axis, 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, Maximum stress at crack tip due to the applied nominal stress, The Distance from the Neutral axis is the distance from the neutral axis to any given fiber and The Maximum Bending Moment is the absolute value of the maximum moment in the unbraced beam segment.
How to calculate Axial Load when Maximum Stress For Short Beams is Given?
Axial Load when Maximum Stress For Short Beams is Given is defined as applying a force on a structure directly along an axis of the structure is calculated using Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)). To calculate Axial Load when Maximum Stress For Short Beams is Given, you need Moment of Inertia (I), Cross sectional area (A), Maximum stress at crack tip m), Distance from the Neutral axis (y) and Maximum Bending Moment (M). With our tool, you need to enter the respective value for Moment of Inertia, Cross sectional area, Maximum stress at crack tip, Distance from the Neutral axis and Maximum Bending Moment and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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