Angle of Oblique plane when Member Subjected to Axial Loading Solution

STEP 0: Pre-Calculation Summary
Formula Used
Theta = (acos(Normal Stress on Oblique Plane/Stress along y Direction))/2
θ = (acos(σθ/σy))/2
This formula uses 2 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)
acos - The inverse cosine function, is the inverse function of the cosine function. It is the function that takes a ratio as an input and returns the angle whose cosine is equal to that ratio., acos(Number)
Variables Used
Theta - (Measured in Radian) - The Theta is the angle subtended by a plane of a body when stress is applied.
Normal Stress on Oblique Plane - (Measured in Pascal) - Normal Stress on Oblique Plane is the stress acting normally to its oblique plane.
Stress along y Direction - (Measured in Pascal) - The Stress along y Direction can be described as axial stress along the given direction.
STEP 1: Convert Input(s) to Base Unit
Normal Stress on Oblique Plane: 54.99 Megapascal --> 54990000 Pascal (Check conversion ​here)
Stress along y Direction: 110 Megapascal --> 110000000 Pascal (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
θ = (acos(σθy))/2 --> (acos(54990000/110000000))/2
Evaluating ... ...
θ = 0.523651260396103
STEP 3: Convert Result to Output's Unit
0.523651260396103 Radian -->30.0030071574084 Degree (Check conversion ​here)
FINAL ANSWER
30.0030071574084 30.00301 Degree <-- Theta
(Calculation completed in 00.004 seconds)

Credits

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Created by Rithik Agrawal
National Institute of Technology Karnataka (NITK), Surathkal
Rithik Agrawal has created this Calculator and 1300+ more calculators!
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Verified by M Naveen
National Institute of Technology (NIT), Warangal
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Stresses of Members Subjected to Axial Loading Calculators

Angle of Oblique plane when Member Subjected to Axial Loading
​ LaTeX ​ Go Theta = (acos(Normal Stress on Oblique Plane/Stress along y Direction))/2
Shear Stress when Member Subjected to Axial Load
​ LaTeX ​ Go Shear Stress on Oblique Plane = 0.5*Stress along y Direction*sin(2*Theta)
Stress along Y-direction when Member Subjected to Axial Load
​ LaTeX ​ Go Stress along y Direction = Normal Stress on Oblique Plane/(cos(2*Theta))
Normal Stress when Member Subjected to Axial Load
​ LaTeX ​ Go Normal Stress on Oblique Plane = Stress along y Direction*cos(2*Theta)

Angle of Oblique plane when Member Subjected to Axial Loading Formula

​LaTeX ​Go
Theta = (acos(Normal Stress on Oblique Plane/Stress along y Direction))/2
θ = (acos(σθ/σy))/2

What is Principal Stress?

Principal stress is the maximum normal stress a body can have at its some point. It represents purely normal stress. If at some point principal stress is said to have acted it does not have any shear stress component.

How to Calculate Angle of Oblique plane when Member Subjected to Axial Loading?

Angle of Oblique plane when Member Subjected to Axial Loading calculator uses Theta = (acos(Normal Stress on Oblique Plane/Stress along y Direction))/2 to calculate the Theta, The Angle of Oblique plane when Member Subjected to Axial Loading formula is defined as calculating the angle of an oblique plane which is being acted upon by normal stress and stress in the x-direction. Theta is denoted by θ symbol.

How to calculate Angle of Oblique plane when Member Subjected to Axial Loading using this online calculator? To use this online calculator for Angle of Oblique plane when Member Subjected to Axial Loading, enter Normal Stress on Oblique Plane θ) & Stress along y Direction y) and hit the calculate button. Here is how the Angle of Oblique plane when Member Subjected to Axial Loading calculation can be explained with given input values -> 1718.873 = (acos(54990000/110000000))/2.

FAQ

What is Angle of Oblique plane when Member Subjected to Axial Loading?
The Angle of Oblique plane when Member Subjected to Axial Loading formula is defined as calculating the angle of an oblique plane which is being acted upon by normal stress and stress in the x-direction and is represented as θ = (acos(σθy))/2 or Theta = (acos(Normal Stress on Oblique Plane/Stress along y Direction))/2. Normal Stress on Oblique Plane is the stress acting normally to its oblique plane & The Stress along y Direction can be described as axial stress along the given direction.
How to calculate Angle of Oblique plane when Member Subjected to Axial Loading?
The Angle of Oblique plane when Member Subjected to Axial Loading formula is defined as calculating the angle of an oblique plane which is being acted upon by normal stress and stress in the x-direction is calculated using Theta = (acos(Normal Stress on Oblique Plane/Stress along y Direction))/2. To calculate Angle of Oblique plane when Member Subjected to Axial Loading, you need Normal Stress on Oblique Plane θ) & Stress along y Direction y). With our tool, you need to enter the respective value for Normal Stress on Oblique Plane & Stress along y Direction 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 Theta?
In this formula, Theta uses Normal Stress on Oblique Plane & Stress along y Direction. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Theta = (arsin(((2*Shear Stress on Oblique Plane)/Stress along y Direction)))/2
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