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

GoNormal Stress across Oblique Section Formula

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

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Normal Stress is stress that occurs when a member is loaded by an axial force. Check FAQs

σ n = \frac{σ 1 + σ 2}{2} + \frac{σ 1 - σ 2}{2}

σ_n - Normal Stress?σ₁ - Major Tensile Stress?σ₂ - Minor Tensile Stress?

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

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Here is how the Normal Stress for Principal Planes when Planes are at Angle of 0 Degree equation looks like with Values.

Here is how the Normal Stress for Principal Planes when Planes are at Angle of 0 Degree equation looks like with Units.

Here is how the Normal Stress for Principal Planes when Planes are at Angle of 0 Degree equation looks like.

124 = \frac{124 + 48}{2} + \frac{124 - 48}{2}

124MPa = \frac{124MPa + 48MPa}{2} + \frac{124MPa - 48MPa}{2}

124 = \frac{124 + 48}{2} + \frac{124 - 48}{2}

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

Follow our step by step solution on how to calculate Normal Stress for Principal Planes when Planes are at Angle of 0 Degree?

FIRST Step Consider the formula

σ n = \frac{σ 1 + σ 2}{2} + \frac{σ 1 - σ 2}{2}

Next Step Substitute values of Variables

∴

σ n = \frac{124MPa + 48MPa}{2} + \frac{124MPa - 48MPa}{2}

Next Step Convert Units

∴

σ n = \frac{1.2E+8Pa + 4.8E+7Pa}{2} + \frac{1.2E+8Pa - 4.8E+7Pa}{2}

Next Step Prepare to Evaluate

∴

σ n = \frac{1.2E+8 + 4.8E+7}{2} + \frac{1.2E+8 - 4.8E+7}{2}

Next Step Evaluate

∴

σ n = 124000000Pa

LAST Step Convert to Output's Unit

∴

σ n = 124MPa

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

Variables

Normal Stress

Normal Stress is stress that occurs when a member is loaded by an axial force.

Symbol: σ_n

Measurement: StressUnit: MPa

Note: Value should be greater than 0.

Formulas to find Normal Stress

Major Tensile Stress

Major Tensile Stress is the stress acting along the longitudinal direction.

Symbol: σ₁

Measurement: PressureUnit: MPa

Note: Value can be positive or negative.

Formulas to find Major Tensile Stress

Minor Tensile Stress

Minor Tensile Stress is the stress acting along lateral direction.

Symbol: σ₂

Measurement: PressureUnit: MPa

Note: Value can be positive or negative.

Formulas to find Minor Tensile Stress

Other Formulas to find Normal Stress

Go Normal Stress across Oblique Section

σ n = σ \cdot {(\cos (θ oblique))}^{2}

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

σ n = \frac{σ 1 + σ 2}{2} + \frac{σ 1 - σ 2}{2}

Go Normal Stress for Principal Planes at Angle of 90 degrees

σ n = \frac{σ 1 + σ 2}{2} - \frac{σ 1 - σ 2}{2}

Go Normal Stress on Oblique Section given Stress in Perpendicular Directions

σ n = \frac{σ 1 + σ 2}{2} + \frac{σ 1 - σ 2}{2} \cdot \cos (2 \cdot θ oblique)

Other formulas in Normal Stress category

Go Equivalent Stress by Distortion Energy Theory

σ e = \frac{1}{\sqrt{2}} \cdot \sqrt{{(σ 1 - σ 2)}^{2} + {(σ 2 - σ 3)}^{2} + {(σ 3 - σ 1)}^{2}}

Go Stress Amplitude

σ a = \frac{σ max - σ min}{2}

How to Evaluate 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 evaluator uses Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2 to evaluate 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 evaluate Normal Stress for Principal Planes when Planes are at Angle of 0 Degree using this online evaluator? To use this online evaluator 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.

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

What is the formula to find Normal Stress for Principal Planes when Planes are at Angle of 0 Degree?

The formula of Normal Stress for Principal Planes when Planes are at Angle of 0 Degree is expressed as Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2. Here is an example- 0.000124 = (124000000+48000000)/2+(124000000-48000000)/2.

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

With Major Tensile Stress (σ₁) & Minor Tensile Stress (σ₂) we can find Normal Stress for Principal Planes when Planes are at Angle of 0 Degree using the formula - Normal Stress = (Major Tensile Stress+Minor Tensile Stress)/2+(Major Tensile Stress-Minor Tensile Stress)/2.

What are the other ways to Calculate Normal Stress?

Here are the different ways to Calculate Normal Stress-

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

Can the Normal Stress for Principal Planes when Planes are at Angle of 0 Degree be negative?

No, the Normal Stress for Principal Planes when Planes are at Angle of 0 Degree, measured in Stress cannot be negative.

Which unit is used to measure 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 is usually measured using the Megapascal[MPa] for Stress. Pascal[MPa], Newton per Square Meter[MPa], Newton per Square Millimeter[MPa] are the few other units in which Normal Stress for Principal Planes when Planes are at Angle of 0 Degree can be measured.

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