Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
Chandana P Dev has created this Calculator and 100+ more calculators!
Mithila Muthamma PA
Coorg Institute of Technology (CIT), Coorg
Mithila Muthamma PA has verified this Calculator and 50+ more calculators!

6 Other formulas that you can solve using the same Inputs

Distance from Middle Surface When Normal Stress is Given
Distance from middle surface=(Shell thickness^(2)/(12*Unit bending moment))*((Normal stress on thin shells*Shell thickness)-(Unit normal force)) GO
Twisting Moments When Shearing Stress is Given
Twisting moments on shells=(((Shearing stress on shells*Shell thickness)-Central shear)*Shell thickness^2)/(12*Distance from middle surface) GO
Shearing Stresses on Shells
Shearing stress on shells=((Central shear/Shell thickness)+(Twisting moments on shells*Distance from middle surface*12/Shell thickness^3)) GO
Central Shear When Shearing Stress is Given
Central shear=(Shearing stress on shells-(12*Twisting moments on shells*Distance from middle surface/Shell thickness^3))*Shell thickness GO
Distance from Middle Surface When Normal Shearing Stress is Given
Distance from middle surface=sqrt((Shell thickness^(2)/4)-((Normal shearing stress*Shell thickness^3)/(6*Unit normal force))) GO
Normal Shearing Stresses
Normal shearing stress=(6*Unit shear force/Shell thickness^(3))*((Shell thickness^(2))/4)-(Distance from middle surface^2) GO

Normal Stress Formula

Normal stress on thin shells=(Unit normal force/Shell thickness)+((Unit bending moment*Distance from middle surface)/(Shell thickness^(3)/12))
f<sub>x</sub>=(N<sub>x</sub>/t)+((M<sub>x</sub>*z)/(t^(3)/12))
More formulas
Distance from Middle Surface When Normal Stress is Given GO
Shearing Stresses on Shells GO
Central Shear When Shearing Stress is Given GO
Twisting Moments When Shearing Stress is Given GO
Normal Shearing Stresses GO
Distance from Middle Surface When Normal Shearing Stress is Given GO

What are Thin Shells?

A Thin Shell is defined as a shell with a thickness which is small compared to its other dimensions and in which deformations are not large compared to thickness. Thin-shell structures are lightweight constructions using shell elements. These elements, typically curved, are assembled to make large structures. Typical applications include aircraft fuselages, boat hulls, and the roofs of large buildings.

How to Calculate Normal Stress?

Normal Stress calculator uses Normal stress on thin shells=(Unit normal force/Shell thickness)+((Unit bending moment*Distance from middle surface)/(Shell thickness^(3)/12)) to calculate the Normal stress on thin shells, The Normal Stress is defined as the perpendicular stress formed on the shell surface due to the normal force acting on it. The force is assumed to be uniformly distributed along the surface of the thin shell. . Normal stress on thin shells and is denoted by fx symbol.

How to calculate Normal Stress using this online calculator? To use this online calculator for Normal Stress, enter Unit normal force (Nx), Shell thickness (t), Unit bending moment (Mx) and Distance from middle surface (z) and hit the calculate button. Here is how the Normal Stress calculation can be explained with given input values -> 0.006005 = (100/20)+((200000*20)/(20^(3)/12)).

FAQ

What is Normal Stress?
The Normal Stress is defined as the perpendicular stress formed on the shell surface due to the normal force acting on it. The force is assumed to be uniformly distributed along the surface of the thin shell. and is represented as fx=(Nx/t)+((Mx*z)/(t^(3)/12)) or Normal stress on thin shells=(Unit normal force/Shell thickness)+((Unit bending moment*Distance from middle surface)/(Shell thickness^(3)/12)). Unit normal force is the force acting perpendicular to the surface in contact with each other whose magnitude is unity. , Shell thickness is the the distance through the shell. , Unit bending moment is the external force or moment acting on a member which allows the member to bend whose magnitude is unity and Distance from middle surface is the half distance from middle surface to extreme surface, say half the thickness. .
How to calculate Normal Stress?
The Normal Stress is defined as the perpendicular stress formed on the shell surface due to the normal force acting on it. The force is assumed to be uniformly distributed along the surface of the thin shell. is calculated using Normal stress on thin shells=(Unit normal force/Shell thickness)+((Unit bending moment*Distance from middle surface)/(Shell thickness^(3)/12)). To calculate Normal Stress, you need Unit normal force (Nx), Shell thickness (t), Unit bending moment (Mx) and Distance from middle surface (z). With our tool, you need to enter the respective value for Unit normal force, Shell thickness, Unit bending moment and 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.
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