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!

11 Other formulas that you can solve using the same Inputs

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
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
Neutral Axis to Outermost Fiber Distance when Total Unit Stress in Eccentric Loading is Given
Outermost Fiber Distance=(Total Unit Stress-(Axial Load/Cross sectional area))*Moment of Inertia about Neutral Axis/(Axial Load*Distance_from Load Applied) GO
Total Unit Stress in Eccentric Loading
Total Unit Stress=(Axial Load/Cross sectional area)+(Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis) GO
Maximum Bending Moment when Maximum Stress For Short Beams is Given
Maximum Bending Moment=((Maximum stress at crack tip-(Axial Load/Cross sectional area))*Moment of Inertia)/Distance from the Neutral axis GO
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
Axial Load when Maximum Stress For Short Beams is Given
Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO
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
Resistance
Resistance=(Resistivity*Length of Conductor)/Cross sectional area GO
Centrifugal Stress
Centrifugal Stress=2*Tensile Stress*Cross sectional area GO
Rate of Flow
Rate of flow=Cross sectional area*Average Velocity GO

Stress at Point y for a Curved Beam Formula

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))))
S=((M)/(A*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
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
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 Stress at Point y for a Curved Beam?

The distribution of stress in a curved flexural member is determined by using the following assumptions. 1 The cross section has an axis of symmetry in a plane along the length of the beam. 2 Plane cross sections remain plane after bending. 3 The modulus of elasticity is the same in tension as in compression.

How to Calculate Stress at Point y for a Curved Beam?

Stress at Point y for a Curved Beam calculator uses 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)))) to calculate the Stress, The Stress at Point y for a Curved Beam formula is defined as Bending Moment of Beam/(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))). Stress and is denoted by S symbol.

How to calculate Stress at Point y for a Curved Beam using this online calculator? To use this online calculator for Stress at Point y for a Curved Beam, enter Bending Moment (M), Cross sectional area (A), 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 Stress at Point y for a Curved Beam calculation can be explained with given input values -> 0.1 = ((10000)/(10*10))*(1+((10)/(25900000*(10+10)))).

FAQ

What is Stress at Point y for a Curved Beam?
The Stress at Point y for a Curved Beam formula is defined as Bending Moment of Beam/(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))) and is represented as S=((M)/(A*R))*(1+((y)/(Z*(R+y)))) or 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)))). 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, 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, 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 Stress at Point y for a Curved Beam?
The Stress at Point y for a Curved Beam formula is defined as Bending Moment of Beam/(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))) is calculated using 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)))). To calculate Stress at Point y for a Curved Beam, you need Bending Moment (M), Cross sectional area (A), 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 , Cross sectional area, 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.
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