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

✖Elongation is defined as the length at breaking point expressed as a percentage of its original length (i.e. length at rest).ⓘ Elongation [δl]			+10% -10%
✖The Length of Tapered Bar is defined as the total length of the Bar.ⓘ Length of Tapered Bar [l]			+10% -10%
✖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.ⓘ Area of Cross-Section [A]			+10% -10%
✖Young's Modulus is a mechanical property of linear elastic solid substances. It describes the relationship between longitudinal stress and longitudinal strain.ⓘ Young's Modulus [E]			+10% -10%

✖The Applied Load SOM is a force imposed on an object by a person or another object.ⓘ Load on Conical Bar with known Elongation due to Self Weight [W_Load]

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

STEP 0: Pre-Calculation Summary

Formula Used

Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus))
W_Load = δl/(l/(6*A*E))
This formula uses 5 Variables

Variables Used

Applied Load SOM - (Measured in Newton) - The Applied Load SOM is a force imposed on an object by a person or another object.
Elongation - (Measured in Meter) - Elongation is defined as the length at breaking point expressed as a percentage of its original length (i.e. length at rest).
Length of Tapered Bar - (Measured in Meter) - The Length of Tapered Bar is defined as the total length of the Bar.
Area of Cross-Section - (Measured in Square Meter) - 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.
Young's Modulus - (Measured in Pascal) - Young's Modulus is a mechanical property of linear elastic solid substances. It describes the relationship between longitudinal stress and longitudinal strain.

STEP 1: Convert Input(s) to Base Unit

Elongation: 0.02 Meter --> 0.02 Meter No Conversion Required
Length of Tapered Bar: 7.8 Meter --> 7.8 Meter No Conversion Required
Area of Cross-Section: 5600 Square Millimeter --> 0.0056 Square Meter (Check conversion here)
Young's Modulus: 20000 Megapascal --> 20000000000 Pascal (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

W_Load = δl/(l/(6*A*E)) --> 0.02/(7.8/(6*0.0056*20000000000))

Evaluating ... ...

W_Load = 1723076.92307692

STEP 3: Convert Result to Output's Unit

1723076.92307692 Newton -->1723.07692307692 Kilonewton (Check conversion here)

FINAL ANSWER

1723.07692307692 ≈ 1723.077 Kilonewton <-- Applied Load SOM

(Calculation completed in 00.004 seconds)

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National Institute of Technology Karnataka (NITK), Surathkal

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

LaTeX Go

Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus))
W_Load = δl/(l/(6*A*E))

What is Tapering Rod?

A Circular rod is basically taper uniformly from one end to another end throughout the length and therefore its one end will be of larger diameter and other end will be of smaller diameter.

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

Load on Conical Bar with known Elongation due to Self Weight calculator uses Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus)) to calculate 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 W_Load symbol.

How to calculate Load on Conical Bar with known Elongation due to Self Weight using this online calculator? To use this online calculator 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. Here is how the Load on Conical Bar with known Elongation due to Self Weight calculation can be explained with given input values -> 1.723077 = 0.02/(7.8/(6*0.0056*20000000000)).

FAQ

What is Load on Conical Bar with known Elongation due to Self Weight?

Load on Conical Bar with known Elongation due to Self Weight is defined as the total load produced by conical rod considering self-weight and is represented as W_Load = δl/(l/(6*A*E)) or Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus)). Elongation is defined as the length at breaking point expressed as a percentage of its original length (i.e. length at rest), The Length of Tapered Bar is defined as the total length of the Bar, 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 & Young's Modulus is a mechanical property of linear elastic solid substances. It describes the relationship between longitudinal stress and longitudinal strain.

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

Load on Conical Bar with known Elongation due to Self Weight is defined as the total load produced by conical rod considering self-weight is calculated using Applied Load SOM = Elongation/(Length of Tapered Bar/(6*Area of Cross-Section*Young's Modulus)). To calculate Load on Conical Bar with known Elongation due to Self Weight, you need Elongation (δl), Length of Tapered Bar (l), Area of Cross-Section (A) & Young's Modulus (E). With our tool, you need to enter the respective value for Elongation, Length of Tapered Bar, Area of Cross-Section & Young's Modulus 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 Applied Load SOM?

In this formula, Applied Load SOM uses Elongation, Length of Tapered Bar, Area of Cross-Section & Young's Modulus. We can use 1 other way(s) to calculate the same, which is/are as follows -

Applied Load SOM = Elongation/(Length/(2*Area of Cross-Section*Young's Modulus))

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