Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities Solution

STEP 0: Pre-Calculation Summary
Formula Used
Temperature of Radiation Shield = (0.5*((Temperature of Plane 1^4)+(Temperature of Plane 2^4)))^(1/4)
T3 = (0.5*((TP1^4)+(TP2^4)))^(1/4)
This formula uses 3 Variables
Variables Used
Temperature of Radiation Shield - (Measured in Kelvin) - Temperature of Radiation Shield is defined as the temperature of radiation shield placed between two parallel infinite plane.
Temperature of Plane 1 - (Measured in Kelvin) - The Temperature of Plane 1 is the degree or intensity of heat present in Plane 1.
Temperature of Plane 2 - (Measured in Kelvin) - The Temperature of Plane 2 is the degree or intensity of heat present in Plane 2.
STEP 1: Convert Input(s) to Base Unit
Temperature of Plane 1: 452 Kelvin --> 452 Kelvin No Conversion Required
Temperature of Plane 2: 445 Kelvin --> 445 Kelvin No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
T3 = (0.5*((TP1^4)+(TP2^4)))^(1/4) --> (0.5*((452^4)+(445^4)))^(1/4)
Evaluating ... ...
T3 = 448.540964702765
STEP 3: Convert Result to Output's Unit
448.540964702765 Kelvin --> No Conversion Required
FINAL ANSWER
448.540964702765 448.541 Kelvin <-- Temperature of Radiation Shield
(Calculation completed in 00.004 seconds)

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University School of Chemical Technology-USCT (GGSIPU), New Delhi
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23 Radiation Formulas Calculators

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
Wavelength Given Speed of Light and Frequency
Go Wavelength = [c]/Frequency
Frequency given Speed of Light and Wavelength
Go Frequency = [c]/Wavelength
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

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

Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities Formula

Temperature of Radiation Shield = (0.5*((Temperature of Plane 1^4)+(Temperature of Plane 2^4)))^(1/4)
T3 = (0.5*((TP1^4)+(TP2^4)))^(1/4)

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 Emissivity?

Emissivity is defined as the ratio of the energy radiated from a material's surface to that radiated from a perfect emitter, known as a blackbody, at the same temperature and wavelength and under the same viewing conditions. It is a dimensionless number between 0 (for a perfect reflector) and 1 (for a perfect emitter).

How to Calculate Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities?

Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities calculator uses Temperature of Radiation Shield = (0.5*((Temperature of Plane 1^4)+(Temperature of Plane 2^4)))^(1/4) to calculate the Temperature of Radiation Shield, The Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities formula is defined as the function of temperature of both the Parallel Infinite Planes in Kelvin . Temperature of Radiation Shield is denoted by T3 symbol.

How to calculate Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities using this online calculator? To use this online calculator for Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities, enter Temperature of Plane 1 (TP1) & Temperature of Plane 2 (TP2) and hit the calculate button. Here is how the Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities calculation can be explained with given input values -> 448.541 = (0.5*((452^4)+(445^4)))^(1/4).

FAQ

What is Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities?
The Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities formula is defined as the function of temperature of both the Parallel Infinite Planes in Kelvin and is represented as T3 = (0.5*((TP1^4)+(TP2^4)))^(1/4) or Temperature of Radiation Shield = (0.5*((Temperature of Plane 1^4)+(Temperature of Plane 2^4)))^(1/4). The Temperature of Plane 1 is the degree or intensity of heat present in Plane 1 & The Temperature of Plane 2 is the degree or intensity of heat present in Plane 2.
How to calculate Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities?
The Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities formula is defined as the function of temperature of both the Parallel Infinite Planes in Kelvin is calculated using Temperature of Radiation Shield = (0.5*((Temperature of Plane 1^4)+(Temperature of Plane 2^4)))^(1/4). To calculate Temperature of Radiation Shield Placed between Two Parallel Infinite Planes with Equal Emissivities, you need Temperature of Plane 1 (TP1) & Temperature of Plane 2 (TP2). With our tool, you need to enter the respective value for Temperature of Plane 1 & Temperature of Plane 2 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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