Normal Stress for Principal Planes at Angle of 90 degrees 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 at Angle of 90 degrees [σ_n]

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Normal Stress for Principal Planes at Angle of 90 degrees 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: 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

σ_n = (σ₁+σ₂)/2-(σ₁-σ₂)/2 --> (1.24E-07+11196)/2-(1.24E-07-11196)/2

Evaluating ... ...

σ_n = 11196

STEP 3: Convert Result to Output's Unit

11196 Pascal -->0.011196 Megapascal (Check conversion here)

FINAL ANSWER

0.011196 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 at Angle of 90 degrees 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 at Angle of 90 degrees?

Normal Stress for Principal Planes at Angle of 90 degrees 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 at Angle of 90 degrees formula is defined as a measure of the normal stress on a plane at a 90-degree angle to the principal planes, providing a critical value for understanding stress distribution and material failure in structural analysis. Normal Stress is denoted by σ_n symbol.

How to calculate Normal Stress for Principal Planes at Angle of 90 degrees using this online calculator? To use this online calculator for Normal Stress for Principal Planes at Angle of 90 degrees, enter Major Tensile Stress (σ₁) & Minor Tensile Stress (σ₂) and hit the calculate button. Here is how the Normal Stress for Principal Planes at Angle of 90 degrees calculation can be explained with given input values -> 1.1E-8 = (1.24E-07+11196)/2-(1.24E-07-11196)/2.

FAQ

What is Normal Stress for Principal Planes at Angle of 90 degrees?

Normal Stress for Principal Planes at Angle of 90 degrees formula is defined as a measure of the normal stress on a plane at a 90-degree angle to the principal planes, providing a critical value for understanding stress distribution and material failure in structural analysis 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 at Angle of 90 degrees?

Normal Stress for Principal Planes at Angle of 90 degrees formula is defined as a measure of the normal stress on a plane at a 90-degree angle to the principal planes, providing a critical value for understanding stress distribution and material failure in structural analysis 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 at Angle of 90 degrees, 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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