Chaplet Area from Unsupported Load Calculator

✖Unsupported load is the load which is not supported by anything.ⓘ Unsupported Load [UL]

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-10%

✖Chaplet Area is the area of chaplet used in mould preparation.ⓘ Chaplet Area from Unsupported Load [a]

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Formula

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Chaplet Area from Unsupported Load

Formula

`"a" = 29*"UL"`

Example

`"2900m²"=29*"100N"`

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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 area of chaplet used in mould preparation.
Unsupported Load - (Measured in Newton) - Unsupported load is the load which is not supported by anything.

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

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

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< 13 Cores - Core Prints and Chaplets Calculators

Buoyant Force on Vertical Cores

Go Buoyant Force = (pi/4*(Diameter of Core Print^2-Diameter of Cylinder^2)*Height of Core Print*Density of Metal-Volume of the Core*Density of Core)*[g]

Buoyant Force on Cylindrical Cores Placed Horizontally

Go Buoyant Force = pi/4*Diameter of Cylinder^2*[g]*Cylinder Height*(Density of Metal-Density of Core)

Metallostatic Forces Acting on Moulding Flasks

Go Metallostatic Force = [g]*Density of Metal*Projected Area in Parting plane*Head of Molten Metal

Density of Core Material

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

Volume of Core

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

Density of Molten Metal

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

Buoyant Force on Cores

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

Chaplet Area

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

Unsupported Load for Cores

Go Unsupported Load = Buoyant Force-Empirical constant*Core Print Area

Buoyant Force on Cores from Chaplet Area

Go Buoyant Force = Chaplet Area/29+Empirical constant*Core Print Area

Empirical Relation for Max. Permissible Buoyancy Force on given Core Print Area

Go Buoyant Force = Empirical constant*Core Print Area

Empirical Relation for Minimum Core Print Area

Go Core Print Area = Buoyant Force/Empirical constant

Chaplet Area from Unsupported Load

Go Chaplet Area = 29*Unsupported Load

Chaplet Area from Unsupported Load Formula

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 load which is not supported by anything.

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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