Alithea Fernandes
Don Bosco College of Engineering (DBCE), Goa
Alithea Fernandes has created this Calculator and 100+ more calculators!
Rudrani Tidke
Cummins College of Engineering for Women (CCEW), Pune
Rudrani Tidke has verified this Calculator and 50+ more calculators!

6 Other formulas that you can solve using the same Inputs

Stress at Point y for a Curved Beam
Stress=((Bending Moment )/(Cross sectional area*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
Bending Moment When Stress is Applied at Point y in a Curved Beam
Bending Moment =((Stress*Cross sectional area*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
Pressure coefficient for slender bodies of revolution
Pressure coefficient=2*(Angle of Deflection^2)+(Curvature of the surface *Distance of Point from Centroidal Axis) GO
Pressure coefficient for slender 2-D bodies
Pressure coefficient=2*((deflection angle^2)+(Curvature of the surface *Distance of Point from Centroidal Axis)) GO
Stress in Tensile Steel when Bending Moment is Given
steel stress=(Bending Moment )/(Area of steel required*Distance between reinforcements) GO
eccentricity between central and neutral axis
Eccentricity=Radius of Centroidal Axis-Radius of neutral axis GO

11 Other formulas that calculate the same Output

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
Cross-Sectional Area when Maximum Stress For Short Beams is Given
Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) 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 Stress is Applied at Point y in a Curved Beam Formula

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))))
A=(M/(S*R))*(1+(y/(Z*(R+y))))
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
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
Axial Load when Maximum Stress For Short Beams is Given 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

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

The cross-sectional area of a curved beam is the area of a two-dimensional shape that is obtained when the curved beam is sliced perpendicular to the centroidal axis at a point y where stress at the point is known.

How to Calculate Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam?

Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam calculator uses 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)))) to calculate the Cross sectional area, The Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam formula is defined as (Bending Moment of Beam/(Stress of Curved Beam*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 and is denoted by A symbol.

How to calculate Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam using this online calculator? To use this online calculator for Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam, enter Bending Moment (M), Stress (S), Radius of Centroidal Axis (R), Distance of Point from Centroidal Axis (y) and Cross-Section Property (Z) and hit the calculate button. Here is how the Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam calculation can be explained with given input values -> 0.1 = (10000/(10000*10))*(1+(10/(25900000*(10+10)))).

FAQ

What is Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam?
The Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam formula is defined as (Bending Moment of Beam/(Stress of Curved Beam*Radius_of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis)))) and is represented as A=(M/(S*R))*(1+(y/(Z*(R+y)))) or 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)))). Bending Moment is the reaction induced in a structural element when an external force or moment is applied to the element, causing the element to bend, Stress at the cross section of curved beam, Radius of Centroidal Axis is the radius of the centroidal axis of the beam, Distance of Point from Centroidal Axis is the distance of a point from the centroidal axis of a curved beam(positive when measured towards the convex side) and Cross-Section Property is the cross section property which can be found using analytical expressions or geometric integration.
How to calculate Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam?
The Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam formula is defined as (Bending Moment of Beam/(Stress of Curved Beam*Radius_of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis)))) is calculated using 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)))). To calculate Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam, you need Bending Moment (M), Stress (S), Radius of Centroidal Axis (R), Distance of Point from Centroidal Axis (y) and Cross-Section Property (Z). With our tool, you need to enter the respective value for Bending Moment , Stress, Radius of Centroidal Axis, Distance of Point from Centroidal Axis and Cross-Section Property 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 Bending Moment , Stress, Radius of Centroidal Axis, Distance of Point from Centroidal Axis and Cross-Section Property. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia))
  • 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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