Normal Stress across Oblique Section Calculator

✖Stress in Bar applied to a bar is the force per unit area applied to the barl. The maximum stress a material can stand before it breaks is called the breaking stress or ultimate tensile stress.ⓘ Stress in Bar [σ]			+10% -10%
✖Angle Made By Oblique Section with Normal cross-section, it is denoted by symbol θ.ⓘ Angle Made By Oblique Section With Normal [θ_o]			+10% -10%

✖Normal Stress is stress that occurs when a member is loaded by an axial force.ⓘ Normal Stress across Oblique Section [σ_n]

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Normal Stress across Oblique Section Solution

STEP 0: Pre-Calculation Summary

Formula Used

Normal Stress = Stress in Bar*(cos(Angle Made By Oblique Section With Normal))^2
σ_n = σ*(cos(θ_o))^2
This formula uses 1 Functions, 3 Variables

Functions Used

cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)

Variables Used

Normal Stress - (Measured in Pascal) - Normal Stress is stress that occurs when a member is loaded by an axial force.
Stress in Bar - (Measured in Pascal) - Stress in Bar applied to a bar is the force per unit area applied to the barl. The maximum stress a material can stand before it breaks is called the breaking stress or ultimate tensile stress.
Angle Made By Oblique Section With Normal - (Measured in Radian) - Angle Made By Oblique Section with Normal cross-section, it is denoted by symbol θ.

STEP 1: Convert Input(s) to Base Unit

Stress in Bar: 0.012 Megapascal --> 12000 Pascal (Check conversion here)
Angle Made By Oblique Section With Normal: 15 Degree --> 0.2617993877991 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

σ_n = σ*(cos(θ_o))^2 --> 12000*(cos(0.2617993877991))^2

Evaluating ... ...

σ_n = 11196.1524227069

STEP 3: Convert Result to Output's Unit

11196.1524227069 Pascal -->0.0111961524227069 Megapascal (Check conversion here)

FINAL ANSWER

0.0111961524227069 ≈ 0.011196 Megapascal <-- Normal Stress

(Calculation completed in 00.004 seconds)

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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 across Oblique Section Formula

LaTeX Go

Normal Stress = Stress in Bar*(cos(Angle Made By Oblique Section With Normal))^2
σ_n = σ*(cos(θ_o))^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 across Oblique Section?

Normal Stress across Oblique Section calculator uses Normal Stress = Stress in Bar*(cos(Angle Made By Oblique Section With Normal))^2 to calculate the Normal Stress, Normal Stress across Oblique Section formula is defined as a measure of the normal stress experienced by an oblique section of a material, which is influenced by the principal stress and the angle of obliquity, providing a critical parameter in evaluating the structural integrity and potential failure of materials under various loads. Normal Stress is denoted by σ_n symbol.

How to calculate Normal Stress across Oblique Section using this online calculator? To use this online calculator for Normal Stress across Oblique Section, enter Stress in Bar (σ) & Angle Made By Oblique Section With Normal (θ_o) and hit the calculate button. Here is how the Normal Stress across Oblique Section calculation can be explained with given input values -> 1.1E-8 = 12000*(cos(0.2617993877991))^2.

FAQ

What is Normal Stress across Oblique Section?

Normal Stress across Oblique Section formula is defined as a measure of the normal stress experienced by an oblique section of a material, which is influenced by the principal stress and the angle of obliquity, providing a critical parameter in evaluating the structural integrity and potential failure of materials under various loads and is represented as σ_n = σ*(cos(θ_o))^2 or Normal Stress = Stress in Bar*(cos(Angle Made By Oblique Section With Normal))^2. Stress in Bar applied to a bar is the force per unit area applied to the barl. The maximum stress a material can stand before it breaks is called the breaking stress or ultimate tensile stress & Angle Made By Oblique Section with Normal cross-section, it is denoted by symbol θ.

How to calculate Normal Stress across Oblique Section?

Normal Stress across Oblique Section formula is defined as a measure of the normal stress experienced by an oblique section of a material, which is influenced by the principal stress and the angle of obliquity, providing a critical parameter in evaluating the structural integrity and potential failure of materials under various loads is calculated using Normal Stress = Stress in Bar*(cos(Angle Made By Oblique Section With Normal))^2. To calculate Normal Stress across Oblique Section, you need Stress in Bar (σ) & Angle Made By Oblique Section With Normal (θ_o). With our tool, you need to enter the respective value for Stress in Bar & Angle Made By Oblique Section With Normal 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 Stress in Bar & Angle Made By Oblique Section With Normal. We can use 3 other way(s) to calculate the same, which is/are as follows -

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

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