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

✖Major Tensile Stress is the stress acting along the longitudinal direction.ⓘ Major Tensile Stress [σ₁]			+10% -10%
✖Minor Tensile Stress is the stress acting along lateral direction.ⓘ Minor Tensile Stress [σ₂]			+10% -10%

✖Normal Stress is stress that occurs when a member is loaded by an axial force.ⓘ Normal Stress for Principal Planes when Planes are at Angle of 0 Degree [σ_n]

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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
σ_n = (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: 124 Megapascal --> 124000000 Pascal (Check conversion here)
Minor Tensile Stress: 48 Megapascal --> 48000000 Pascal (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

σ_n = (σ₁+σ₂)/2+(σ₁-σ₂)/2 --> (124000000+48000000)/2+(124000000-48000000)/2

Evaluating ... ...

σ_n = 124000000

STEP 3: Convert Result to Output's Unit

124000000 Pascal -->124 Megapascal (Check conversion here)

FINAL ANSWER

124 Megapascal <-- Normal Stress

(Calculation completed in 00.004 seconds)

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Institute of Aeronautical Engineering (IARE), Hyderabad

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< Normal Stress Calculators

Normal Stress for Principal Planes at Angle of 0 Degrees given Major and Minor Tensile Stress

LaTeX 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

LaTeX 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

LaTeX Go Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2-(Major Tensile Stress-Minor Tensile Stress)/2

Normal Stress across Oblique Section

LaTeX 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

LaTeX Go

Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2
σ_n = (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, The Normal Stress for Principal Planes when Planes are at Angle of 0 Degree formula is defined as the sum of average of major tensile stress, minor tensile stress and half of difference between major tensile stress, minor tensile stress. Normal Stress is denoted by σ_n 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 (σ₁) & Minor Tensile Stress (σ₂) 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 -> 0.000124 = (124000000+48000000)/2+(124000000-48000000)/2.

FAQ

What is Normal Stress for Principal Planes when Planes are at Angle of 0 Degree?

The Normal Stress for Principal Planes when Planes are at Angle of 0 Degree formula is defined as the sum of average of major tensile stress, minor tensile stress and half of difference between major tensile stress, minor tensile stress and is represented as σ_n = (σ₁+σ₂)/2+(σ₁-σ₂)/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?

The Normal Stress for Principal Planes when Planes are at Angle of 0 Degree formula is defined as the sum of average of major tensile stress, minor tensile stress and half of difference between major tensile stress, minor tensile stress 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 (σ₁) & Minor Tensile Stress (σ₂). 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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