Normal Stress for Principal Planes when Planes are at Angle of 0 Degree Solution

STEP 0: Pre-Calculation Summary
Formula Used
Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2
σn = (σ1+σ2)/2+(σ1-σ2)/2
This formula uses 3 Variables
Variables Used
Normal Stress - (Measured in Pascal) - Normal Stress is stress that occurs when a member is loaded by an axial force.
Major Tensile Stress - (Measured in Pascal) - Major Tensile Stress is the stress acting along the longitudinal direction.
Minor Tensile Stress - (Measured in Pascal) - Minor Tensile Stress is the stress acting along lateral direction.
STEP 1: Convert Input(s) to Base Unit
Major Tensile Stress: 1.24E-07 Newton per Square Meter --> 1.24E-07 Pascal (Check conversion ​here)
Minor Tensile Stress: 11196 Newton per Square Meter --> 11196 Pascal (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σn = (σ12)/2+(σ12)/2 --> (1.24E-07+11196)/2+(1.24E-07-11196)/2
Evaluating ... ...
σn = 1.24000507639721E-07
STEP 3: Convert Result to Output's Unit
1.24000507639721E-07 Pascal -->1.24000507639721E-13 Megapascal (Check conversion ​here)
FINAL ANSWER
1.24000507639721E-13 1.2E-13 Megapascal <-- Normal Stress
(Calculation completed in 00.020 seconds)

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Normal Stress Calculators

Normal Stress for Principal Planes at Angle of 0 Degrees given Major and Minor Tensile Stress
​ Go Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2
Normal Stress for Principal Planes when Planes are at Angle of 0 Degree
​ Go Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2
Normal Stress for Principal Planes at Angle of 90 degrees
​ Go Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2-(Major Tensile Stress-Minor Tensile Stress)/2
Normal Stress across Oblique Section
​ Go Normal Stress = Stress in Bar*(cos(Angle Made By Oblique Section With Normal))^2

Normal Stress for Principal Planes when Planes are at Angle of 0 Degree Formula

​Go
Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2
σn = (σ1+σ2)/2+(σ1-σ2)/2

What is normal stress?

Stress is said to be normal stress when the direction of the deforming force is perpendicular to the cross-sectional area of the body.

How to Calculate Normal Stress for Principal Planes when Planes are at Angle of 0 Degree?

Normal Stress for Principal Planes when Planes are at Angle of 0 Degree calculator uses Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2 to calculate the Normal Stress, Normal Stress for Principal Planes when Planes are at Angle of 0 Degree formula is defined as the average of the maximum and minimum normal stresses on a plane, providing a crucial parameter in understanding the stress distribution on a material under different loading conditions. Normal Stress is denoted by σn symbol.

How to calculate Normal Stress for Principal Planes when Planes are at Angle of 0 Degree using this online calculator? To use this online calculator for Normal Stress for Principal Planes when Planes are at Angle of 0 Degree, enter Major Tensile Stress 1) & Minor Tensile Stress 2) and hit the calculate button. Here is how the Normal Stress for Principal Planes when Planes are at Angle of 0 Degree calculation can be explained with given input values -> 1.2E-19 = (1.24E-07+11196)/2+(1.24E-07-11196)/2.

FAQ

What is Normal Stress for Principal Planes when Planes are at Angle of 0 Degree?
Normal Stress for Principal Planes when Planes are at Angle of 0 Degree formula is defined as the average of the maximum and minimum normal stresses on a plane, providing a crucial parameter in understanding the stress distribution on a material under different loading conditions and is represented as σn = (σ12)/2+(σ12)/2 or Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2. Major Tensile Stress is the stress acting along the longitudinal direction & Minor Tensile Stress is the stress acting along lateral direction.
How to calculate Normal Stress for Principal Planes when Planes are at Angle of 0 Degree?
Normal Stress for Principal Planes when Planes are at Angle of 0 Degree formula is defined as the average of the maximum and minimum normal stresses on a plane, providing a crucial parameter in understanding the stress distribution on a material under different loading conditions is calculated using Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2. To calculate Normal Stress for Principal Planes when Planes are at Angle of 0 Degree, you need Major Tensile Stress 1) & Minor Tensile Stress 2). With our tool, you need to enter the respective value for Major Tensile Stress & Minor Tensile Stress 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 Normal Stress?
In this formula, Normal Stress uses Major Tensile Stress & Minor Tensile Stress. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Normal Stress = Stress in Bar*(cos(Angle Made By Oblique Section With Normal))^2
  • Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2
  • Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2-(Major Tensile Stress-Minor Tensile Stress)/2
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