## < ⎙ 11 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
Heat Transfer by Conduction at Base
Heat transfer=((Thermal Conductivity*Cross sectional area*Perimeter*Heat transfer coefficient)^0.5)*(Base Temperature-Ambient Temperature) 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
Current for a Moving Coil Galvanometer
Electric Current=(Spring constant*Angle of Deflection)/(Number of Turns of a coil*Cross sectional area*Magnetic Field) 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

### Direct Stress Formula

Direct Stress=Axial Thrust/Cross sectional area
More formulas
Young's Modulus GO
Bulk Modulus GO
Factor of Safety GO
Strain Energy Density GO
Shear strength for double parallel fillet weld GO
Shear Stress GO
Bulk Stress GO
Tensile Strain GO
Shear Strain GO
Bulk Strain GO
Bulk Modulus GO
Elastic Modulus GO
Shear Modulus GO
Brinell Hardness Number GO
Shear Strain GO
Axial elongation of prismatic bar due to external load GO
Elongation of prismatic bar due to its own weight GO
Elongation circular tapered bar GO
Strain energy due to pure shear GO
Strain Energy if moment value is given GO
Strain Energy if Torsion Moment Value is Given GO
Strain Energy if applied tension load is given GO
Deflection of fixed beam with load at center GO
Hooke's law GO
Poisson's Ratio GO
Longitudinal strain GO
Lateral Strain GO
Volumetric Strain GO
Volumetric Strain GO
Deflection of fixed beam with uniformly distributed load GO
Thermal Stress GO
Thermal Stress in tapered bar GO
Section Modulus GO
Shearing Stress GO
Maximum Shearing Stress GO
Shear Stress of Circular Beam GO
Bending Stress GO
Torsional Shear Stress GO
Equivalent Torsional Moment GO
Equivalent Bending Moment GO
Slenderness Ratio GO
Rankine's Formula for Columns GO
Total Angle of Twist GO
Moment of Inertia about Polar Axis GO
Moment of Inertia for Hollow Circular Shaft GO
Strain Energy in Torsion GO
Strain Energy due to Torsion in Hollow Shaft GO
Strain Energy in Torsion for Solid Shaft GO

## What is Direct Stress?

The Direct Stress is the stress produced by the axial force acting on a unit area.Whenever a body is subjected to an axial tension or compression, a direct stress comes into play at every section of body.

## How to Calculate Direct Stress?

Direct Stress calculator uses Direct Stress=Axial Thrust/Cross sectional area to calculate the Direct Stress, The Direct Stress is defined as the stress produced by the axial force acting on a unit area.It is also called as normal stress. Direct Stress and is denoted by 𝛔 symbol.

How to calculate Direct Stress using this online calculator? To use this online calculator for Direct Stress, enter Cross sectional area (A) and Axial Thrust (P) and hit the calculate button. Here is how the Direct Stress calculation can be explained with given input values -> 5 = 50/10.

### FAQ

What is Direct Stress?
The Direct Stress is defined as the stress produced by the axial force acting on a unit area.It is also called as normal stress and is represented as 𝛔=P/A or Direct Stress=Axial Thrust/Cross sectional area. 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 and The Axial Thrust is the resultant force of all the axial forces (F) acting on the object or material.
How to calculate Direct Stress?
The Direct Stress is defined as the stress produced by the axial force acting on a unit area.It is also called as normal stress is calculated using Direct Stress=Axial Thrust/Cross sectional area. To calculate Direct Stress, you need Cross sectional area (A) and Axial Thrust (P). With our tool, you need to enter the respective value for Cross sectional area and Axial Thrust 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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