Chaplet Area from Unsupported Load Calculator

✖Unsupported Load is the force applied to a structure or component without any external support or reinforcement.ⓘ Unsupported Load [UL]

+10%

-10%

✖Chaplet Area is the surface area of a chaplet, a metal support used in casting to prevent deformation or distortion of the casting mold.ⓘ Chaplet Area from Unsupported Load [a]

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Chaplet Area from Unsupported Load Solution

STEP 0: Pre-Calculation Summary

Formula Used

Chaplet Area = 29*Unsupported Load
a = 29*UL
This formula uses 2 Variables

Variables Used

Chaplet Area - (Measured in Square Meter) - Chaplet Area is the surface area of a chaplet, a metal support used in casting to prevent deformation or distortion of the casting mold.
Unsupported Load - (Measured in Newton) - Unsupported Load is the force applied to a structure or component without any external support or reinforcement.

STEP 1: Convert Input(s) to Base Unit

Unsupported Load: 100 Newton --> 100 Newton No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

a = 29*UL --> 29*100

Evaluating ... ...

a = 2900

STEP 3: Convert Result to Output's Unit

2900 Square Meter --> No Conversion Required

FINAL ANSWER

2900 Square Meter <-- Chaplet Area

(Calculation completed in 00.004 seconds)

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Created by Rajat Vishwakarma

University Institute of Technology RGPV (UIT - RGPV), Bhopal

Rajat Vishwakarma has created this Calculator and 400+ more calculators!

Verified by Nishan Poojary

Shri Madhwa Vadiraja Institute of Technology and Management (SMVITM), Udupi

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< Cores Core Prints and Chaplets Calculators

Density of Core Material

LaTeX Go Density of Core = Density of Core Metal-Buoyant Force/(Volume of The Core*[g])

Volume of Core

LaTeX Go Volume of The Core = Buoyant Force/(9.81*(Density of Core Metal-Density of Core))

Density of Molten Metal

LaTeX Go Density of Core Metal = Buoyant Force/(Volume of The Core*9.81)+Density of Core

Buoyant Force on Cores

LaTeX Go Buoyant Force = 9.81*Volume of The Core*(Density of Core Metal-Density of Core)

Chaplet Area from Unsupported Load Formula

LaTeX Go

Chaplet Area = 29*Unsupported Load
a = 29*UL

What are chaplets?

Chaplets are metallic supports often kept inside the mould cavity to support the cores. These are of the same composition as that of the pouring metal so that the molten metal would provide enough heat to completely melt them and thus fuse with it during solidification.

How to Calculate Chaplet Area from Unsupported Load?

Chaplet Area from Unsupported Load calculator uses Chaplet Area = 29*Unsupported Load to calculate the Chaplet Area, Chaplet area from unsupported load is the area of chaplets required for supporting the cores in order to prevent shifting due to other forces. Chaplet Area is denoted by a symbol.

How to calculate Chaplet Area from Unsupported Load using this online calculator? To use this online calculator for Chaplet Area from Unsupported Load, enter Unsupported Load (UL) and hit the calculate button. Here is how the Chaplet Area from Unsupported Load calculation can be explained with given input values -> 2900 = 29*100.

FAQ

What is Chaplet Area from Unsupported Load?

Chaplet area from unsupported load is the area of chaplets required for supporting the cores in order to prevent shifting due to other forces and is represented as a = 29*UL or Chaplet Area = 29*Unsupported Load. Unsupported Load is the force applied to a structure or component without any external support or reinforcement.

How to calculate Chaplet Area from Unsupported Load?

Chaplet area from unsupported load is the area of chaplets required for supporting the cores in order to prevent shifting due to other forces is calculated using Chaplet Area = 29*Unsupported Load. To calculate Chaplet Area from Unsupported Load, you need Unsupported Load (UL). With our tool, you need to enter the respective value for Unsupported Load 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 Chaplet Area?

In this formula, Chaplet Area uses Unsupported Load. We can use 1 other way(s) to calculate the same, which is/are as follows -

Chaplet Area = 29*(Buoyant Force-Empirical Constant*Core Print Area)

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