Stress Due to Direct Load given Maximum Stress for Failure of Long Column Solution

STEP 0: Pre-Calculation Summary
Formula Used
Direct Stress = Maximum Stress-Column Bending Stress
σ = σmax-σb
This formula uses 3 Variables
Variables Used
Direct Stress - (Measured in Pascal) - Direct Stress is defined as axial thrust acting per unit area.
Maximum Stress - (Measured in Pascal) - Maximum Stress is the maximum stress that a material withstands before fracture.
Column Bending Stress - (Measured in Pascal) - Column Bending Stress is the normal stress that is induced at a point in a body subjected to loads that cause it to bend.
STEP 1: Convert Input(s) to Base Unit
Maximum Stress: 0.00506 Megapascal --> 5060 Pascal (Check conversion here)
Column Bending Stress: 0.005 Megapascal --> 5000 Pascal (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σ = σmaxb --> 5060-5000
Evaluating ... ...
σ = 60
STEP 3: Convert Result to Output's Unit
60 Pascal -->6E-05 Megapascal (Check conversion here)
FINAL ANSWER
6E-05 6E-5 Megapascal <-- Direct Stress
(Calculation completed in 00.004 seconds)

Credits

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National Institute Of Technology (NIT), Hamirpur
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15 Failure of a Column Calculators

Section Modulus about Axis of Bending for Long Column
Go Section Modulus = (Column Compressive Load*Column Maximum Bending)/Column Bending Stress
Area of Cross-Section given Compressive Stress Induced during Failure of Short Column
Go Column Cross Sectional Area = Column Compressive Load/Column Compressive Stress
Compressive Load given Compressive Stress Induced during Failure of Short Column
Go Column Compressive Load = Column Cross Sectional Area*Column Compressive Stress
Compressive Stress Induced during Failure of Short Column
Go Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area
Area of Cross-Section given Stress due to Direct Load for Long Column
Go Column Cross Sectional Area = Column Compressive Load/Direct Stress
Compressive Load given Stress Due to Direct Load for Long Column
Go Column Compressive Load = Column Cross Sectional Area*Direct Stress
Stress Due to Direct Load for Long Column
Go Direct Stress = Column Compressive Load/Column Cross Sectional Area
Area of Cross Section of Column given Crushing Stress
Go Column Cross Sectional Area = Crushing load/Column Crushing Stress
Crushing Stress for Short Column
Go Column Crushing Stress = Crushing load/Column Cross Sectional Area
Crushing Load for Short Column
Go Crushing load = Column Cross Sectional Area*Column Crushing Stress
Stress Due to Bending at Center of Column given Minimum Stress for Failure of Long Column
Go Column Bending Stress = Minimum Stress Value-Direct Stress
Minimum Stress for Failure of Long Column
Go Minimum Stress Value = Direct Stress+Column Bending Stress
Stress Due to Bending at Center of Column given Maximum Stress for Failure of Long Column
Go Column Bending Stress = Maximum Stress-Direct Stress
Stress Due to Direct Load given Maximum Stress for Failure of Long Column
Go Direct Stress = Maximum Stress-Column Bending Stress
Maximum Stress for Failure of Long Column
Go Maximum Stress = Direct Stress+Column Bending Stress

15 Modes of Failure in Eccentric Compression Calculators

Section Modulus about Axis of Bending for Long Column
Go Section Modulus = (Column Compressive Load*Column Maximum Bending)/Column Bending Stress
Area of Cross-Section given Compressive Stress Induced during Failure of Short Column
Go Column Cross Sectional Area = Column Compressive Load/Column Compressive Stress
Compressive Load given Compressive Stress Induced during Failure of Short Column
Go Column Compressive Load = Column Cross Sectional Area*Column Compressive Stress
Compressive Stress Induced during Failure of Short Column
Go Column Compressive Stress = Column Compressive Load/Column Cross Sectional Area
Area of Cross-Section given Stress due to Direct Load for Long Column
Go Column Cross Sectional Area = Column Compressive Load/Direct Stress
Compressive Load given Stress Due to Direct Load for Long Column
Go Column Compressive Load = Column Cross Sectional Area*Direct Stress
Stress Due to Direct Load for Long Column
Go Direct Stress = Column Compressive Load/Column Cross Sectional Area
Area of Cross Section of Column given Crushing Stress
Go Column Cross Sectional Area = Crushing load/Column Crushing Stress
Crushing Stress for Short Column
Go Column Crushing Stress = Crushing load/Column Cross Sectional Area
Crushing Load for Short Column
Go Crushing load = Column Cross Sectional Area*Column Crushing Stress
Stress Due to Bending at Center of Column given Minimum Stress for Failure of Long Column
Go Column Bending Stress = Minimum Stress Value-Direct Stress
Minimum Stress for Failure of Long Column
Go Minimum Stress Value = Direct Stress+Column Bending Stress
Stress Due to Bending at Center of Column given Maximum Stress for Failure of Long Column
Go Column Bending Stress = Maximum Stress-Direct Stress
Stress Due to Direct Load given Maximum Stress for Failure of Long Column
Go Direct Stress = Maximum Stress-Column Bending Stress
Maximum Stress for Failure of Long Column
Go Maximum Stress = Direct Stress+Column Bending Stress

Stress Due to Direct Load given Maximum Stress for Failure of Long Column Formula

Direct Stress = Maximum Stress-Column Bending Stress
σ = σmax-σb

Where is Bending Stress Maximum?

The bottom die has a large deflection due to the bending force. The maximum bending stress occurs at the top surface of the die, and its location is corresponding to the inner bumps of the bottom die. The deflection of the beam is proportional to the bending moment, which is also proportional to the bending force.

How to Calculate Stress Due to Direct Load given Maximum Stress for Failure of Long Column?

Stress Due to Direct Load given Maximum Stress for Failure of Long Column calculator uses Direct Stress = Maximum Stress-Column Bending Stress to calculate the Direct Stress, The Stress Due to Direct Load given Maximum Stress for Failure of Long Column formula is defined as the stress which is normal to the plane on which they act and they are either tensile or compressive. Direct Stress is denoted by σ symbol.

How to calculate Stress Due to Direct Load given Maximum Stress for Failure of Long Column using this online calculator? To use this online calculator for Stress Due to Direct Load given Maximum Stress for Failure of Long Column, enter Maximum Stress max) & Column Bending Stress b) and hit the calculate button. Here is how the Stress Due to Direct Load given Maximum Stress for Failure of Long Column calculation can be explained with given input values -> -3E-9 = 5060-5000.

FAQ

What is Stress Due to Direct Load given Maximum Stress for Failure of Long Column?
The Stress Due to Direct Load given Maximum Stress for Failure of Long Column formula is defined as the stress which is normal to the plane on which they act and they are either tensile or compressive and is represented as σ = σmaxb or Direct Stress = Maximum Stress-Column Bending Stress. Maximum Stress is the maximum stress that a material withstands before fracture & Column Bending Stress is the normal stress that is induced at a point in a body subjected to loads that cause it to bend.
How to calculate Stress Due to Direct Load given Maximum Stress for Failure of Long Column?
The Stress Due to Direct Load given Maximum Stress for Failure of Long Column formula is defined as the stress which is normal to the plane on which they act and they are either tensile or compressive is calculated using Direct Stress = Maximum Stress-Column Bending Stress. To calculate Stress Due to Direct Load given Maximum Stress for Failure of Long Column, you need Maximum Stress max) & Column Bending Stress b). With our tool, you need to enter the respective value for Maximum Stress & Column Bending 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 Direct Stress?
In this formula, Direct Stress uses Maximum Stress & Column Bending Stress. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Direct Stress = Column Compressive Load/Column Cross Sectional Area
  • Direct Stress = Column Compressive Load/Column Cross Sectional Area
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