Normal Stress using Obliquity Solution

STEP 0: Pre-Calculation Summary
Formula Used
Normal Stress = Shear Stress/tan(Angle of Obliquity)
σn = 𝜏/tan(ϕ)
This formula uses 1 Functions, 3 Variables
Functions Used
tan - The tangent of an angle is a trigonometric ratio of the length of the side opposite an angle to the length of the side adjacent to an angle in a right triangle., tan(Angle)
Variables Used
Normal Stress - (Measured in Pascal) - Normal Stress is stress that occurs when a member is loaded by an axial force.
Shear Stress - (Measured in Pascal) - Shear Stress is force tending to cause deformation of a material by slippage along a plane or planes parallel to the imposed stress.
Angle of Obliquity - (Measured in Radian) - The Angle of Obliquity is the angle made by resultant stress with the normal of the oblique plane.
STEP 1: Convert Input(s) to Base Unit
Shear Stress: 2.4 Megapascal --> 2400000 Pascal (Check conversion ​here)
Angle of Obliquity: 45 Degree --> 0.785398163397301 Radian (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σn = 𝜏/tan(ϕ) --> 2400000/tan(0.785398163397301)
Evaluating ... ...
σn = 2400000.00000071
STEP 3: Convert Result to Output's Unit
2400000.00000071 Pascal -->2.40000000000071 Megapascal (Check conversion ​here)
FINAL ANSWER
2.40000000000071 2.4 Megapascal <-- Normal Stress
(Calculation completed in 00.004 seconds)

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Created by Chilvera Bhanu Teja
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 using Obliquity Formula

​LaTeX ​Go
Normal Stress = Shear Stress/tan(Angle of Obliquity)
σn = 𝜏/tan(ϕ)

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 using Obliquity?

Normal Stress using Obliquity calculator uses Normal Stress = Shear Stress/tan(Angle of Obliquity) to calculate the Normal Stress, Normal Stress using Obliquity formula is defined as a measure of the normal stress on a plane at an angle to the principal plane, which is essential in understanding the principal stresses and their role in structural analysis and material failure. Normal Stress is denoted by σn symbol.

How to calculate Normal Stress using Obliquity using this online calculator? To use this online calculator for Normal Stress using Obliquity, enter Shear Stress (𝜏) & Angle of Obliquity (ϕ) and hit the calculate button. Here is how the Normal Stress using Obliquity calculation can be explained with given input values -> 2.4E-6 = 2400000/tan(0.785398163397301).

FAQ

What is Normal Stress using Obliquity?
Normal Stress using Obliquity formula is defined as a measure of the normal stress on a plane at an angle to the principal plane, which is essential in understanding the principal stresses and their role in structural analysis and material failure and is represented as σn = 𝜏/tan(ϕ) or Normal Stress = Shear Stress/tan(Angle of Obliquity). Shear Stress is force tending to cause deformation of a material by slippage along a plane or planes parallel to the imposed stress & The Angle of Obliquity is the angle made by resultant stress with the normal of the oblique plane.
How to calculate Normal Stress using Obliquity?
Normal Stress using Obliquity formula is defined as a measure of the normal stress on a plane at an angle to the principal plane, which is essential in understanding the principal stresses and their role in structural analysis and material failure is calculated using Normal Stress = Shear Stress/tan(Angle of Obliquity). To calculate Normal Stress using Obliquity, you need Shear Stress (𝜏) & Angle of Obliquity (ϕ). With our tool, you need to enter the respective value for Shear Stress & Angle of Obliquity 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 Shear Stress & Angle of Obliquity. 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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