Net Heat Exchange between Two Surfaces given Radiosity for Both Surface Solution

STEP 0: Pre-Calculation Summary
Formula Used
Radiation Heat Transfer = (Radiosity of 1st Body-Radiosity of 2nd Body)/(1/(Surface Area of Body 1*Radiation Shape Factor 12))
q1-2 = (J1-J2)/(1/(A1*F12))
This formula uses 5 Variables
Variables Used
Radiation Heat Transfer - (Measured in Watt) - Radiation Heat Transfer is the amount of heat that is transferred per unit of time in some material, usually measured in watts (joules per second).
Radiosity of 1st Body - (Measured in Watt per Square Meter) - Radiosity of 1st Body represents the rate at which radiation energy leaves a unit area of a surface in all directions.
Radiosity of 2nd Body - (Measured in Watt per Square Meter) - Radiosity of 2nd Body represents the rate at which radiation energy leaves a unit area of a surface in all directions.
Surface Area of Body 1 - (Measured in Square Meter) - The Surface Area of Body 1 is the area of body 1 through which the radiation takes place.
Radiation Shape Factor 12 - Radiation Shape Factor 12 is the fraction of radiation energy radiated by one surface which is incident on another surface when both surfaces are placed in a non-absorbing medium.
STEP 1: Convert Input(s) to Base Unit
Radiosity of 1st Body: 61 Watt per Square Meter --> 61 Watt per Square Meter No Conversion Required
Radiosity of 2nd Body: 49 Watt per Square Meter --> 49 Watt per Square Meter No Conversion Required
Surface Area of Body 1: 34.74 Square Meter --> 34.74 Square Meter No Conversion Required
Radiation Shape Factor 12: 0.59 --> No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
q1-2 = (J1-J2)/(1/(A1*F12)) --> (61-49)/(1/(34.74*0.59))
Evaluating ... ...
q1-2 = 245.9592
STEP 3: Convert Result to Output's Unit
245.9592 Watt --> No Conversion Required
FINAL ANSWER
245.9592 Watt <-- Radiation Heat Transfer
(Calculation completed in 00.005 seconds)

Credits

Created by Ayush gupta
University School of Chemical Technology-USCT (GGSIPU), New Delhi
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10+ Radiation Heat Transfer Calculators

Heat Transfer between Concentric Spheres
Go Heat Transfer = (Surface Area of Body 1*[Stefan-BoltZ]*((Temperature of Surface 1^4)-(Temperature of Surface 2^4)))/((1/Emissivity of Body 1)+(((1/Emissivity of Body 2)-1)*((Radius of Smaller Sphere/Radius of Larger Sphere)^2)))
Heat Transfer between Two Long Concentric Cylinder given Temp, Emissivity and Area of Both Surfaces
Go Heat Transfer = (([Stefan-BoltZ]*Surface Area of Body 1*((Temperature of Surface 1^4)-(Temperature of Surface 2^4))))/((1/Emissivity of Body 1)+((Surface Area of Body 1/Surface Area of Body 2)*((1/Emissivity of Body 2)-1)))
Radiation Heat Transfer between Plane 1 and Shield given Temperature and Emissivity of Both Surfaces
Go Heat Transfer = Area*[Stefan-BoltZ]*((Temperature of Plane 1^4)-(Temperature of Radiation Shield^4))/((1/Emissivity of Body 1)+(1/Emissivity of Radiation Shield)-1)
Radiation Heat Transfer between Plane 2 and Radiation Shield given Temperature and Emissivity
Go Heat Transfer = Area*[Stefan-BoltZ]*((Temperature of Radiation Shield^4)-(Temperature of Plane 2^4))/ ((1/Emissivity of Radiation Shield)+(1/Emissivity of Body 2)-1)
Heat Transfer between Two Infinite Parallel Planes given Temp and Emissivity of Both Surfaces
Go Heat Transfer = (Area*[Stefan-BoltZ]*((Temperature of Surface 1^4)-(Temperature of Surface 2^4)))/ ((1/Emissivity of Body 1)+(1/Emissivity of Body 2)-1)
Heat Transfer between Small Convex Object in Large Enclosure
Go Heat Transfer = Surface Area of Body 1*Emissivity of Body 1*[Stefan-BoltZ]*((Temperature of Surface 1^4)-(Temperature of Surface 2^4))
Net Heat Exchange given Area 1 and Shape Factor 12
Go Net Heat Transfer = Surface Area of Body 1*Radiation Shape Factor 12*(Emissive Power of 1st Blackbody-Emissive Power of 2nd Blackbody)
Net Heat Exchange given Area 2 and Shape Factor 21
Go Net Heat Transfer = Surface Area of Body 2*Radiation Shape Factor 21*(Emissive Power of 1st Blackbody-Emissive Power of 2nd Blackbody)
Net Heat Exchange between Two Surfaces given Radiosity for Both Surface
Go Radiation Heat Transfer = (Radiosity of 1st Body-Radiosity of 2nd Body)/(1/(Surface Area of Body 1*Radiation Shape Factor 12))
Net Heat Transfer from Surface given Emissivity, Radiosity and Emissive Power
Go Heat Transfer = (((Emissivity*Area)*(Emissive Power of Blackbody-Radiosity))/(1-Emissivity))

25 Important Formulas in Radiation Heat Transfer Calculators

Heat Transfer between Concentric Spheres
Go Heat Transfer = (Surface Area of Body 1*[Stefan-BoltZ]*((Temperature of Surface 1^4)-(Temperature of Surface 2^4)))/((1/Emissivity of Body 1)+(((1/Emissivity of Body 2)-1)*((Radius of Smaller Sphere/Radius of Larger Sphere)^2)))
Heat Transfer between Small Convex Object in Large Enclosure
Go Heat Transfer = Surface Area of Body 1*Emissivity of Body 1*[Stefan-BoltZ]*((Temperature of Surface 1^4)-(Temperature of Surface 2^4))
Radiosity given Emissive Power and Irradiation
Go Radiosity = (Emissivity*Emissive Power of Blackbody)+(Reflectivity*Irradiation)
Area of Surface 1 given Area 2 and Radiation Shape Factor for Both Surfaces
Go Surface Area of Body 1 = Surface Area of Body 2*(Radiation Shape Factor 21/Radiation Shape Factor 12)
Area of Surface 2 given Area 1 and Radiation Shape Factor for Both Surfaces
Go Surface Area of Body 2 = Surface Area of Body 1*(Radiation Shape Factor 12/Radiation Shape Factor 21)
Shape Factor 12 given Area of Both Surface and Shape Factor 21
Go Radiation Shape Factor 12 = (Surface Area of Body 2/Surface Area of Body 1)*Radiation Shape Factor 21
Shape Factor 21 given Area of Both Surface and Shape Factor 12
Go Radiation Shape Factor 21 = Radiation Shape Factor 12*(Surface Area of Body 1/Surface Area of Body 2)
Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities
Go Temperature of Radiation Shield = (0.5*((Temperature of Plane 1^4)+(Temperature of Plane 2^4)))^(1/4)
Emissive Power of Blackbody
Go Emissive Power of Blackbody = [Stefan-BoltZ]*(Temperature of Blackbody^4)
Net Energy Leaving given Radiosity and Irradiation
Go Heat Transfer = Area*(Radiosity-Irradiation)
Emissive Power of Non Blackbody given Emissivity
Go Emissive Power of Non Blackbody = Emissivity*Emissive Power of Blackbody
Emissivity of Body
Go Emissivity = Emissive Power of Non Blackbody/Emissive Power of Blackbody
Total Resistance in Radiation Heat Transfer given Emissivity and Number of Shields
Go Resistance = (Number of Shields+1)*((2/Emissivity)-1)
Reflected Radiation given Absorptivity and Transmissivity
Go Reflectivity = 1-Absorptivity-Transmissivity
Absorptivity given Reflectivity and Transmissivity
Go Absorptivity = 1-Reflectivity-Transmissivity
Transmissivity Given Reflectivity and Absorptivity
Go Transmissivity = 1-Absorptivity-Reflectivity
Mass of Particle Given Frequency and Speed of Light
Go Mass of Particle = [hP]*Frequency/([c]^2)
Energy of each Quanta
Go Energy of Each Quanta = [hP]*Frequency
Frequency given Speed of Light and Wavelength
Go Frequency = [c]/Wavelength
Wavelength Given Speed of Light and Frequency
Go Wavelength = [c]/Frequency
Radiation Temperature given Maximum Wavelength
Go Radiation Temperature = 2897.6/Maximum Wavelength
Maximum Wavelength at given Temperature
Go Maximum Wavelength = 2897.6/Radiation Temperature
Resistance in Radiation Heat Transfer when No Shield is Present and Equal Emissivities
Go Resistance = (2/Emissivity)-1
Reflectivity given Absorptivity for Blackbody
Go Reflectivity = 1-Absorptivity
Reflectivity given Emissivity for Blackbody
Go Reflectivity = 1-Emissivity

Net Heat Exchange between Two Surfaces given Radiosity for Both Surface Formula

Radiation Heat Transfer = (Radiosity of 1st Body-Radiosity of 2nd Body)/(1/(Surface Area of Body 1*Radiation Shape Factor 12))
q1-2 = (J1-J2)/(1/(A1*F12))

What is Radiation?

Radiation is energy that comes from a source and travels through space at the speed of light. This energy has an electric field and a magnetic field associated with it, and has wave-like properties. You could also call radiation “electromagnetic waves”.

What is Blackbody?

A black body is defined as the body which absorbs all the electromagnetic radiation (that is light) that strikes it irrespective of the angle of incidence and frequency of the radiation.

How to Calculate Net Heat Exchange between Two Surfaces given Radiosity for Both Surface?

Net Heat Exchange between Two Surfaces given Radiosity for Both Surface calculator uses Radiation Heat Transfer = (Radiosity of 1st Body-Radiosity of 2nd Body)/(1/(Surface Area of Body 1*Radiation Shape Factor 12)) to calculate the Radiation Heat Transfer, The Net Heat Exchange Between Two Surfaces given Radiosity for Both Surface formula is defined as the function of surface area of 1st surface, shape factor and radiosity of both the surfaces. Radiation Heat Transfer is denoted by q1-2 symbol.

How to calculate Net Heat Exchange between Two Surfaces given Radiosity for Both Surface using this online calculator? To use this online calculator for Net Heat Exchange between Two Surfaces given Radiosity for Both Surface, enter Radiosity of 1st Body (J1), Radiosity of 2nd Body (J2), Surface Area of Body 1 (A1) & Radiation Shape Factor 12 (F12) and hit the calculate button. Here is how the Net Heat Exchange between Two Surfaces given Radiosity for Both Surface calculation can be explained with given input values -> 245.9592 = (61-49)/(1/(34.74*0.59)).

FAQ

What is Net Heat Exchange between Two Surfaces given Radiosity for Both Surface?
The Net Heat Exchange Between Two Surfaces given Radiosity for Both Surface formula is defined as the function of surface area of 1st surface, shape factor and radiosity of both the surfaces and is represented as q1-2 = (J1-J2)/(1/(A1*F12)) or Radiation Heat Transfer = (Radiosity of 1st Body-Radiosity of 2nd Body)/(1/(Surface Area of Body 1*Radiation Shape Factor 12)). Radiosity of 1st Body represents the rate at which radiation energy leaves a unit area of a surface in all directions, Radiosity of 2nd Body represents the rate at which radiation energy leaves a unit area of a surface in all directions, The Surface Area of Body 1 is the area of body 1 through which the radiation takes place & Radiation Shape Factor 12 is the fraction of radiation energy radiated by one surface which is incident on another surface when both surfaces are placed in a non-absorbing medium.
How to calculate Net Heat Exchange between Two Surfaces given Radiosity for Both Surface?
The Net Heat Exchange Between Two Surfaces given Radiosity for Both Surface formula is defined as the function of surface area of 1st surface, shape factor and radiosity of both the surfaces is calculated using Radiation Heat Transfer = (Radiosity of 1st Body-Radiosity of 2nd Body)/(1/(Surface Area of Body 1*Radiation Shape Factor 12)). To calculate Net Heat Exchange between Two Surfaces given Radiosity for Both Surface, you need Radiosity of 1st Body (J1), Radiosity of 2nd Body (J2), Surface Area of Body 1 (A1) & Radiation Shape Factor 12 (F12). With our tool, you need to enter the respective value for Radiosity of 1st Body, Radiosity of 2nd Body, Surface Area of Body 1 & Radiation Shape Factor 12 and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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