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The Applied Load SOM is a force imposed on an object by a person or another object. Check FAQs
WLoad=δll6AE
WLoad - Applied Load SOM?δl - Elongation?l - Length of Tapered Bar?A - Area of Cross-Section?E - Young's Modulus?

Load on Conical Bar with known Elongation due to Self Weight Example

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With units
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Here is how the Load on Conical Bar with known Elongation due to Self Weight equation looks like with Values.

Here is how the Load on Conical Bar with known Elongation due to Self Weight equation looks like with Units.

Here is how the Load on Conical Bar with known Elongation due to Self Weight equation looks like.

1723.0769Edit=0.02Edit7.8Edit65600Edit20000Edit
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Load on Conical Bar with known Elongation due to Self Weight Solution

Follow our step by step solution on how to calculate Load on Conical Bar with known Elongation due to Self Weight?

FIRST Step Consider the formula
WLoad=δll6AE
Next Step Substitute values of Variables
WLoad=0.02m7.8m65600mm²20000MPa
Next Step Convert Units
WLoad=0.02m7.8m60.00562E+10Pa
Next Step Prepare to Evaluate
WLoad=0.027.860.00562E+10
Next Step Evaluate
WLoad=1723076.92307692N
Next Step Convert to Output's Unit
WLoad=1723.07692307692kN
LAST Step Rounding Answer
WLoad=1723.0769kN

Load on Conical Bar with known Elongation due to Self Weight Formula Elements

Variables
Applied Load SOM
The Applied Load SOM is a force imposed on an object by a person or another object.
Symbol: WLoad
Measurement: ForceUnit: kN
Note: Value can be positive or negative.
Elongation
Elongation is defined as the length at breaking point expressed as a percentage of its original length (i.e. length at rest).
Symbol: δl
Measurement: LengthUnit: m
Note: Value can be positive or negative.
Length of Tapered Bar
The Length of Tapered Bar is defined as the total length of the Bar.
Symbol: l
Measurement: LengthUnit: m
Note: Value can be positive or negative.
Area of Cross-Section
Area of Cross-section is a cross-sectional area which we obtain when the same object is cut into two pieces. The area of that particular cross-section is known as the cross-sectional area.
Symbol: A
Measurement: AreaUnit: mm²
Note: Value should be greater than 0.
Young's Modulus
Young's Modulus is a mechanical property of linear elastic solid substances. It describes the relationship between longitudinal stress and longitudinal strain.
Symbol: E
Measurement: StressUnit: MPa
Note: Value can be positive or negative.

Other Formulas to find Applied Load SOM

​Go Load on Prismatic Bar with known Elongation due to Self Weight
WLoad=δlL2AE

Other formulas in Elongation of Tapering Bar due to Self Weight category

​Go Length of Circular Tapering Rod when deflection due to load
L=δl4WLoadπE(d1d2)
​Go Self Weight of Prismatic Bar with known Elongation
γ=δlLLE2
​Go Modulus of Elasticity of Prismatic Bar with known Elongation due to Self Weight
E=γLLδl2
​Go Length of Prismatic Rod given Elongation due to Self Weight in Uniform Bar
L=δlWLoad2AE

How to Evaluate Load on Conical Bar with known Elongation due to Self Weight?

Load on Conical Bar with known Elongation due to Self Weight evaluator uses Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus)) to evaluate the Applied Load SOM, Load on Conical Bar with known Elongation due to Self Weight is defined as the total load produced by conical rod considering self-weight. Applied Load SOM is denoted by WLoad symbol.

How to evaluate Load on Conical Bar with known Elongation due to Self Weight using this online evaluator? To use this online evaluator for Load on Conical Bar with known Elongation due to Self Weight, enter Elongation (δl), Length of Tapered Bar (l), Area of Cross-Section (A) & Young's Modulus (E) and hit the calculate button.

FAQs on Load on Conical Bar with known Elongation due to Self Weight

What is the formula to find Load on Conical Bar with known Elongation due to Self Weight?
The formula of Load on Conical Bar with known Elongation due to Self Weight is expressed as Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus)). Here is an example- 1.723077 = 0.02/(7.8/(6*0.0056*20000000000)).
How to calculate Load on Conical Bar with known Elongation due to Self Weight?
With Elongation (δl), Length of Tapered Bar (l), Area of Cross-Section (A) & Young's Modulus (E) we can find Load on Conical Bar with known Elongation due to Self Weight using the formula - Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus)).
What are the other ways to Calculate Applied Load SOM?
Here are the different ways to Calculate Applied Load SOM-
  • Applied Load SOM=Elongation/(Length/(2*Area of Cross-Section*Young's Modulus))OpenImg
Can the Load on Conical Bar with known Elongation due to Self Weight be negative?
Yes, the Load on Conical Bar with known Elongation due to Self Weight, measured in Force can be negative.
Which unit is used to measure Load on Conical Bar with known Elongation due to Self Weight?
Load on Conical Bar with known Elongation due to Self Weight is usually measured using the Kilonewton[kN] for Force. Newton[kN], Exanewton[kN], Meganewton[kN] are the few other units in which Load on Conical Bar with known Elongation due to Self Weight can be measured.
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