Chaplet Area Calculator

✖Buoyant Force is the upward force exerted by any fluid upon a body placed in it.ⓘ Buoyant Force [F_buoyant]			+10% -10%
✖Empirical constant is the constant used in an empirical relation. It may have some units.ⓘ Empirical constant [c]			+10% -10%
✖Core print area is the area of that part of the mould which supports the weight of core used in casting.ⓘ Core Print Area [A]			+10% -10%

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

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Formula

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Chaplet Area

Formula

`"a" = 29*("F"_{"buoyant "}-"c"*"A")`

Example

`"2900m²"=29*("1500.0N"-"350N/mm²"*"0.000004m²")`

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Chaplet Area Solution

STEP 0: Pre-Calculation Summary

Formula Used

Chaplet Area = 29*(Buoyant Force-Empirical constant*Core Print Area)
a = 29*(F_buoyant-c*A)
This formula uses 4 Variables

Variables Used

Chaplet Area - (Measured in Square Meter) - Chaplet Area is the area of chaplet used in mould preparation.
Buoyant Force - (Measured in Newton) - Buoyant Force is the upward force exerted by any fluid upon a body placed in it.
Empirical constant - (Measured in Pascal) - Empirical constant is the constant used in an empirical relation. It may have some units.
Core Print Area - (Measured in Square Meter) - Core print area is the area of that part of the mould which supports the weight of core used in casting.

STEP 1: Convert Input(s) to Base Unit

Buoyant Force: 1500 Newton --> 1500 Newton No Conversion Required
Empirical constant: 350 Newton per Square Millimeter --> 350000000 Pascal (Check conversion here)
Core Print Area: 4E-06 Square Meter --> 4E-06 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

a = 29*(F_buoyant-c*A) --> 29*(1500-350000000*4E-06)

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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Credits

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

Nishan Poojary has verified this Calculator and 400+ more calculators!

< 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 Formula

Chaplet Area = 29*(Buoyant Force-Empirical constant*Core Print Area)
a = 29*(F_buoyant-c*A)

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?

Chaplet Area calculator uses Chaplet Area = 29*(Buoyant Force-Empirical constant*Core Print Area) to calculate the Chaplet Area, The Chaplet area can be defined as the area of the metal pieces used to support the cores during casting. Chaplet Area is denoted by a symbol.

How to calculate Chaplet Area using this online calculator? To use this online calculator for Chaplet Area, enter Buoyant Force (F_buoyant), Empirical constant (c) & Core Print Area (A) and hit the calculate button. Here is how the Chaplet Area calculation can be explained with given input values -> 2900 = 29*(1500-350000000*4E-06).

FAQ

What is Chaplet Area?

The Chaplet area can be defined as the area of the metal pieces used to support the cores during casting and is represented as a = 29*(F_buoyant-c*A) or Chaplet Area = 29*(Buoyant Force-Empirical constant*Core Print Area). Buoyant Force is the upward force exerted by any fluid upon a body placed in it, Empirical constant is the constant used in an empirical relation. It may have some units & Core print area is the area of that part of the mould which supports the weight of core used in casting.

How to calculate Chaplet Area?

The Chaplet area can be defined as the area of the metal pieces used to support the cores during casting is calculated using Chaplet Area = 29*(Buoyant Force-Empirical constant*Core Print Area). To calculate Chaplet Area, you need Buoyant Force (F_buoyant), Empirical constant (c) & Core Print Area (A). With our tool, you need to enter the respective value for Buoyant Force, Empirical constant & Core Print Area 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 Buoyant Force, Empirical constant & Core Print Area. We can use 1 other way(s) to calculate the same, which is/are as follows -

Chaplet Area = 29*Unsupported Load

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