Heat Exchange by Radiation due to Geometric Arrangement Solution

STEP 0: Pre-Calculation Summary
Formula Used
Heat Flux = Emissivity*Cross Sectional Area*[Stefan-BoltZ]*Shape Factor*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4))
q = ε*A*[Stefan-BoltZ]*SF*(T1^(4)-T2^(4))
This formula uses 1 Constants, 6 Variables
Constants Used
[Stefan-BoltZ] - Stefan-Boltzmann Constant Value Taken As 5.670367E-8
Variables Used
Heat Flux - (Measured in Watt per Square Meter) - The Heat Flux is the rate of thermal energy transfer per unit area, indicating how much heat is being transferred through a surface in a given time.
Emissivity - The Emissivity is a measure of a material's ability to emit thermal radiation compared to a perfect black body, influencing heat transfer in thermal systems.
Cross Sectional Area - (Measured in Square Meter) - The Cross Sectional Area is the area of a cut surface through a solid object, influencing fluid flow and heat transfer in thermodynamic applications.
Shape Factor - The Shape Factor is a dimensionless quantity that characterizes the geometric configuration of an object, influencing heat transfer efficiency in conduction, convection, and radiation processes.
Temperature of Surface 1 - (Measured in Kelvin) - The Temperature of Surface 1 is the measure of heat present on the first surface in a thermal system, influencing heat transfer through conduction, convection, and radiation.
Temperature of Surface 2 - (Measured in Kelvin) - The Temperature of Surface 2 is the thermal state of the second surface in a heat transfer system, influencing heat flow and energy exchange.
STEP 1: Convert Input(s) to Base Unit
Emissivity: 0.95 --> No Conversion Required
Cross Sectional Area: 41 Square Meter --> 41 Square Meter No Conversion Required
Shape Factor: 1.000001 --> No Conversion Required
Temperature of Surface 1: 101.01 Kelvin --> 101.01 Kelvin No Conversion Required
Temperature of Surface 2: 91.114 Kelvin --> 91.114 Kelvin No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
q = ε*A*[Stefan-BoltZ]*SF*(T1^(4)-T2^(4)) --> 0.95*41*[Stefan-BoltZ]*1.000001*(101.01^(4)-91.114^(4))
Evaluating ... ...
q = 77.7041695370823
STEP 3: Convert Result to Output's Unit
77.7041695370823 Watt per Square Meter --> No Conversion Required
FINAL ANSWER
77.7041695370823 77.70417 Watt per Square Meter <-- Heat Flux
(Calculation completed in 00.004 seconds)

Credits

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Created by Kethavath Srinath
Osmania University (OU), Hyderabad
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Vishwakarma Government Engineering College (VGEC), Ahmedabad
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Conduction, Convection and Radiation Calculators

Heat Exchange by Radiation due to Geometric Arrangement
​ Go Heat Flux = Emissivity*Cross Sectional Area*[Stefan-BoltZ]*Shape Factor*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4))
Heat Transfer According to Fourier's Law
​ Go Heat Flow Through a Body = -(Thermal Conductivity of Fin*Surface Area of Heat Flow*Temperature Difference/Thickness of The Body)
Convective Processes Heat Transfer Coefficient
​ Go Heat Flux = Heat Transfer Coefficient*(Surface Temperature-Recovery Temperature)
Thermal Resistance in Convection Heat Transfer
​ Go Thermal Resistance = 1/(Exposed Surface Area*Coefficient of Convective Heat Transfer)

Heat Emission due to Radiation Calculators

Heat Exchange by Radiation due to Geometric Arrangement
​ Go Heat Flux = Emissivity*Cross Sectional Area*[Stefan-BoltZ]*Shape Factor*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4))
Black Bodies Heat Exchange by Radiation
​ Go Heat Flux = Emissivity*[Stefan-BoltZ]*Cross Sectional Area*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4))
Non Ideal Body Surface Emittance
​ Go Real Surface Radiant Surface Emittance = Emissivity*[Stefan-BoltZ]*Surface Temperature^(4)
Radiation energy emitted by black body per unit time and surface area
​ LaTeX ​ Go Heat Flux = [Stefan-BoltZ]*Temperature^4

Heat Exchange by Radiation due to Geometric Arrangement Formula

​Go
Heat Flux = Emissivity*Cross Sectional Area*[Stefan-BoltZ]*Shape Factor*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4))
q = ε*A*[Stefan-BoltZ]*SF*(T1^(4)-T2^(4))

what do you mean by heat transfer?

Heat transfer, any or all of several kinds of phenomena, considered as mechanisms, that convey energy and entropy from one location to another. The specific mechanisms are usually referred to as convection, thermal radiation, and conduction.

How to Calculate Heat Exchange by Radiation due to Geometric Arrangement?

Heat Exchange by Radiation due to Geometric Arrangement calculator uses Heat Flux = Emissivity*Cross Sectional Area*[Stefan-BoltZ]*Shape Factor*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4)) to calculate the Heat Flux, Heat Exchange by Radiation due to Geometric Arrangement formula is defined as a measure of the rate of heat transfer between two objects due to their geometric arrangement, taking into account the emissivity, surface area, and temperature difference between the objects. Heat Flux is denoted by q symbol.

How to calculate Heat Exchange by Radiation due to Geometric Arrangement using this online calculator? To use this online calculator for Heat Exchange by Radiation due to Geometric Arrangement, enter Emissivity (ε), Cross Sectional Area (A), Shape Factor (SF), Temperature of Surface 1 (T1) & Temperature of Surface 2 (T2) and hit the calculate button. Here is how the Heat Exchange by Radiation due to Geometric Arrangement calculation can be explained with given input values -> 77.69632 = 0.95*41*[Stefan-BoltZ]*1.000001*(101.01^(4)-91.114^(4)).

FAQ

What is Heat Exchange by Radiation due to Geometric Arrangement?
Heat Exchange by Radiation due to Geometric Arrangement formula is defined as a measure of the rate of heat transfer between two objects due to their geometric arrangement, taking into account the emissivity, surface area, and temperature difference between the objects and is represented as q = ε*A*[Stefan-BoltZ]*SF*(T1^(4)-T2^(4)) or Heat Flux = Emissivity*Cross Sectional Area*[Stefan-BoltZ]*Shape Factor*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4)). The Emissivity is a measure of a material's ability to emit thermal radiation compared to a perfect black body, influencing heat transfer in thermal systems, The Cross Sectional Area is the area of a cut surface through a solid object, influencing fluid flow and heat transfer in thermodynamic applications, The Shape Factor is a dimensionless quantity that characterizes the geometric configuration of an object, influencing heat transfer efficiency in conduction, convection, and radiation processes, The Temperature of Surface 1 is the measure of heat present on the first surface in a thermal system, influencing heat transfer through conduction, convection, and radiation & The Temperature of Surface 2 is the thermal state of the second surface in a heat transfer system, influencing heat flow and energy exchange.
How to calculate Heat Exchange by Radiation due to Geometric Arrangement?
Heat Exchange by Radiation due to Geometric Arrangement formula is defined as a measure of the rate of heat transfer between two objects due to their geometric arrangement, taking into account the emissivity, surface area, and temperature difference between the objects is calculated using Heat Flux = Emissivity*Cross Sectional Area*[Stefan-BoltZ]*Shape Factor*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4)). To calculate Heat Exchange by Radiation due to Geometric Arrangement, you need Emissivity (ε), Cross Sectional Area (A), Shape Factor (SF), Temperature of Surface 1 (T1) & Temperature of Surface 2 (T2). With our tool, you need to enter the respective value for Emissivity, Cross Sectional Area, Shape Factor, Temperature of Surface 1 & Temperature of Surface 2 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 Heat Flux?
In this formula, Heat Flux uses Emissivity, Cross Sectional Area, Shape Factor, Temperature of Surface 1 & Temperature of Surface 2. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Heat Flux = Heat Transfer Coefficient*(Surface Temperature-Recovery Temperature)
  • Heat Flux = Heat Transfer Coefficient*(Surface Temperature-Temperature of Characteristic Fluid)
  • Heat Flux = Emissivity*[Stefan-BoltZ]*Cross Sectional Area*(Temperature of Surface 1^(4)-Temperature of Surface 2^(4))
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