Normal Shearing Stresses Solution

STEP 0: Pre-Calculation Summary
Formula Used
Normal Shearing Stress = ((6*Unit Shear Force)/Shell Thickness^(3))*(((Shell Thickness^(2))/4)-(Distance from Middle Surface^2))
vxz = ((6*V)/t^(3))*(((t^(2))/4)-(z^2))
This formula uses 4 Variables
Variables Used
Normal Shearing Stress - (Measured in Pascal) - Normal Shearing Stress is the shearing stress produced by the normal shearing force.
Unit Shear Force - (Measured in Newton) - Unit Shear Force is the force acting on the shell surface which cause slipping deformation but with a magnitude of unity.
Shell Thickness - (Measured in Meter) - Shell thickness is the the distance through the shell.
Distance from Middle Surface - (Measured in Meter) - Distance from Middle Surface is the half distance from middle surface to extreme surface, say half the thickness.
STEP 1: Convert Input(s) to Base Unit
Unit Shear Force: 100 Kilonewton --> 100000 Newton (Check conversion ​here)
Shell Thickness: 200 Millimeter --> 0.2 Meter (Check conversion ​here)
Distance from Middle Surface: 0.02 Meter --> 0.02 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
vxz = ((6*V)/t^(3))*(((t^(2))/4)-(z^2)) --> ((6*100000)/0.2^(3))*(((0.2^(2))/4)-(0.02^2))
Evaluating ... ...
vxz = 720000
STEP 3: Convert Result to Output's Unit
720000 Pascal -->0.72 Megapascal (Check conversion ​here)
FINAL ANSWER
0.72 Megapascal <-- Normal Shearing Stress
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
Chandana P Dev has created this Calculator and 500+ more calculators!
Verifier Image
Verified by Mithila Muthamma PA
Coorg Institute of Technology (CIT), Coorg
Mithila Muthamma PA has verified this Calculator and 700+ more calculators!

Stresses in Thin Shells Calculators

Distance from Middle Surface given Normal Stress in Thin Shells
​ LaTeX ​ Go Distance from Middle Surface = (Shell Thickness^(2)/(12*Unit Bending Moment))*((Normal Stress on Thin Shells*Shell Thickness)-(Unit Normal Force))
Normal Stress in Thin Shells
​ LaTeX ​ Go Normal Stress on Thin Shells = (Unit Normal Force/Shell Thickness)+((Unit Bending Moment*Distance from Middle Surface)/(Shell Thickness^(3)/12))
Shearing Stresses on Shells
​ LaTeX ​ Go Shearing Stress on Shells = ((Central Shear/Shell Thickness)+((Twisting Moments on Shells*Distance from Middle Surface*12)/Shell Thickness^3))
Central Shear given Shearing Stress
​ LaTeX ​ Go Central Shear = (Shearing Stress on Shells-((Twisting Moments on Shells*Distance from Middle Surface*12)/Shell Thickness^3))*Shell Thickness

Normal Shearing Stresses Formula

​LaTeX ​Go
Normal Shearing Stress = ((6*Unit Shear Force)/Shell Thickness^(3))*(((Shell Thickness^(2))/4)-(Distance from Middle Surface^2))
vxz = ((6*V)/t^(3))*(((t^(2))/4)-(z^2))

What is Normal Stress?

The Normal Stress is a result of load applied perpendicular to a member. Shear stress however results when a load is applied parallel to an area. If in case the shear force acting is normal to the surface, normal stress occurs.

What is Twisting and Torsion?

The twisting moment is also called a torsional moment or torque. When we twist the end of the bar either clockwise or counterclockwise then a bending moment will form. one end twists relative to the other end and each element in a cross-section is in a state of shear. The shearing stresses thereby induced in the shaft produce a moment of resistance, equal and opposite to the applied torque.
The twisting or wrenching of a body by the exertion of forces tending to turn one end or part about a longitudinal axis while the other is held fast or turned in the opposite direction. In the case of a Torque, the force is tangential, and the distance is the radial distance between this tangent and the axis of rotation.

How to Calculate Normal Shearing Stresses?

Normal Shearing Stresses calculator uses Normal Shearing Stress = ((6*Unit Shear Force)/Shell Thickness^(3))*(((Shell Thickness^(2))/4)-(Distance from Middle Surface^2)) to calculate the Normal Shearing Stress, The Normal Shearing Stresses formula is defined as the shear stress provided by the shell against the shearing deformation caused due to shear forces (in normal direction). Normal Shearing Stress is denoted by vxz symbol.

How to calculate Normal Shearing Stresses using this online calculator? To use this online calculator for Normal Shearing Stresses, enter Unit Shear Force (V), Shell Thickness (t) & Distance from Middle Surface (z) and hit the calculate button. Here is how the Normal Shearing Stresses calculation can be explained with given input values -> -29999250000 = ((6*100000)/0.2^(3))*(((0.2^(2))/4)-(0.02^2)).

FAQ

What is Normal Shearing Stresses?
The Normal Shearing Stresses formula is defined as the shear stress provided by the shell against the shearing deformation caused due to shear forces (in normal direction) and is represented as vxz = ((6*V)/t^(3))*(((t^(2))/4)-(z^2)) or Normal Shearing Stress = ((6*Unit Shear Force)/Shell Thickness^(3))*(((Shell Thickness^(2))/4)-(Distance from Middle Surface^2)). Unit Shear Force is the force acting on the shell surface which cause slipping deformation but with a magnitude of unity, Shell thickness is the the distance through the shell & Distance from Middle Surface is the half distance from middle surface to extreme surface, say half the thickness.
How to calculate Normal Shearing Stresses?
The Normal Shearing Stresses formula is defined as the shear stress provided by the shell against the shearing deformation caused due to shear forces (in normal direction) is calculated using Normal Shearing Stress = ((6*Unit Shear Force)/Shell Thickness^(3))*(((Shell Thickness^(2))/4)-(Distance from Middle Surface^2)). To calculate Normal Shearing Stresses, you need Unit Shear Force (V), Shell Thickness (t) & Distance from Middle Surface (z). With our tool, you need to enter the respective value for Unit Shear Force, Shell Thickness & Distance from Middle Surface and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!