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Heat Transfer in an Isobaric Process Calculator

Category Engineering ↺
Engineering Chemical Engineering ↺
Chemical-Engineering Thermodynamics ↺
Thermodynamics Ideal Gas ↺
✖Number of Moles is the amount of gas present in moles. 1 mole of gas weighs as much as its molecular weight.ⓘ Number of Moles [n]
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✖Molar Specific Heat Capacity at Constant Pressure , Cp ( of a gas ) is the amount of heat required to raise the temperature of 1 mol of the gas by 1 °C at the constant volume.ⓘ Molar Specific Heat Capacity at Constant Pressure [Cp]
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-10%
✖Temperature Difference is the measure of the hotness or the coldness of an object.ⓘ Temperature Difference [dT]
+10%
-10%
✖Heat is the form of energy that is transferred between systems or objects with different temperatures (flowing from the high-temperature system to the low-temperature system). Also referred to as heat energy or thermal energy. Heat is typically measured in Btu, calories or joules.ⓘ Heat Transfer in an Isobaric Process [Q]
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Ishan Gupta
Birla Institute of Technology & Science (BITS), Pilani
Ishan Gupta has created this Calculator and 50+ more calculators!

11 Other formulas that you can solve using the same Inputs

Work done in adiabatic process
Work =(Initial Pressure of System*Initial Volume of System-Final Pressure of System*Final Volume of System)/(Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume-1) GO
Final Temperature in Adiabatic Process (using pressure)
final temp.=initial temp.*(Final Pressure of System/Initial Pressure of System)^(1-1/(Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume)) GO
Final Temperature in Adiabatic Process (using volume)
final temp.=initial temp.*(Final Volume of System/Initial Volume of System)^(1-Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume) GO
Adiabatic Index
Heat Capacity Ratio=Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume GO
Change in Internal Energy of the system
Internal Energy=Number of Moles*Molar Specific Heat Capacity at Constant Volume*Temperature Difference GO
Specific Heat Capacity at Constant Volume
Molar Specific Heat Capacity at Constant Volume=Molar Specific Heat Capacity at Constant Pressure-[R] GO
Enthalpy of the system
Enthalpy=Number of Moles*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference GO
Heat Transfer in an Isochoric Process
Heat=Number of Moles*Molar Specific Heat Capacity at Constant Volume*Temperature Difference GO
Partial pressure of Water Vapour
partial pressure=Pressure of Gas*1.8*Atmospheric Pressure*Temperature Difference/2700 GO
Heat Rate
Heat Rate=Steam Flow*Specific Heat Capacity*Temperature Difference GO
Work done in an isobaric process
Work =Number of Moles*[R]*Temperature Difference GO

8 Other formulas that calculate the same Output

Radial Heat flowing through a cylinder
Heat=(Thermal Conductivity*2*pi*(outer radius-inner radius)*Temperature Difference*length of cylinder)/((ln(outer radius/inner radius))*(outer radius-inner radius)) GO
Heat Transfer in a Heat Exchanger using cold fluid properties
Heat=Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Cold Fluid-Outlet Temperature of Cold Fluid) GO
Heat Transfer in a Heat Exchanger using hot fluid properties
Heat=Mass of hot fluid*Specific Heat Capacity of Hot Fluid*(Inlet Temperature of Hot Fluid-Outlet Temperature of Hot Fluid) GO
Radiative Heat Transfer
Heat=[Stefan-BoltZ]*Body Surface Area*Geometric View Factor*(Temperature of surface 1^4-Temperature of surface 2^4) GO
Heat Transfer in an Isochoric Process
Heat=Number of Moles*Molar Specific Heat Capacity at Constant Volume*Temperature Difference GO
Heat Transfer in a Heat Exchanger using overall heat transfer coefficient
Heat=Overall Heat Transfer Coefficient*Area*(Outside Temperature-Inside Temperature) GO
Heat transferred in isothermal process (using pressure)
Heat=[R]*Temperature of Gas*ln(Initial Pressure of System/Final Pressure of System) GO
Heat transferred in isothermal process (using volume)
Heat=[R]*Temperature of Gas*ln(Final Volume of System/Initial Volume of System) GO

Heat Transfer in an Isobaric Process Formula

Heat=Number of Moles*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference
More formulas
Heat Transfer in an Isochoric Process GO
Change in Internal Energy of the system GO
Enthalpy of the system GO
Specific Heat Capacity at Constant Pressure GO
Specific Heat Capacity at Constant Volume GO
Work done in an isobaric process GO
Work done in isothermal process (using pressure) GO
Work done in isothermal process (using volume) GO
Heat transferred in isothermal process (using pressure) GO
Heat transferred in isothermal process (using volume) GO
Work done in adiabatic process GO
Adiabatic Index GO
Final Temperature in Adiabatic Process (using volume) GO
Final Temperature in Adiabatic Process (using pressure) GO

What Is Heat Transfer in an Isobaric Process?

Heat Transfer in an Isobaric Process gives the amount of heat transferred in bringing the system to its final state from its initial state at constant pressure conditions.

How to Calculate Heat Transfer in an Isobaric Process?

Heat Transfer in an Isobaric Process calculator uses Heat=Number of Moles*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference to calculate the Heat, Heat Transfer in an Isobaric Process gives the amount of heat transferred in bringing the system to its final state from its initial state at constant pressure conditions. Heat and is denoted by Q symbol.

How to calculate Heat Transfer in an Isobaric Process using this online calculator? To use this online calculator for Heat Transfer in an Isobaric Process, enter Temperature Difference (dT), Number of Moles (n) and Molar Specific Heat Capacity at Constant Pressure (Cp) and hit the calculate button. Here is how the Heat Transfer in an Isobaric Process calculation can be explained with given input values -> 20 = 1*1*20.

FAQ

What is Heat Transfer in an Isobaric Process?
Heat Transfer in an Isobaric Process gives the amount of heat transferred in bringing the system to its final state from its initial state at constant pressure conditions and is represented as Q=n*Cp*dT or Heat=Number of Moles*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference. Temperature Difference is the measure of the hotness or the coldness of an object, Number of Moles is the amount of gas present in moles. 1 mole of gas weighs as much as its molecular weight and Molar Specific Heat Capacity at Constant Pressure , Cp ( of a gas ) is the amount of heat required to raise the temperature of 1 mol of the gas by 1 °C at the constant volume.
How to calculate Heat Transfer in an Isobaric Process?
Heat Transfer in an Isobaric Process gives the amount of heat transferred in bringing the system to its final state from its initial state at constant pressure conditions is calculated using Heat=Number of Moles*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference. To calculate Heat Transfer in an Isobaric Process, you need Temperature Difference (dT), Number of Moles (n) and Molar Specific Heat Capacity at Constant Pressure (Cp). With our tool, you need to enter the respective value for Temperature Difference, Number of Moles and Molar Specific Heat Capacity at Constant Pressure 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?
In this formula, Heat uses Temperature Difference, Number of Moles and Molar Specific Heat Capacity at Constant Pressure. We can use 8 other way(s) to calculate the same, which is/are as follows -
  • Heat=Overall Heat Transfer Coefficient*Area*(Outside Temperature-Inside Temperature)
  • Heat=Mass of Cold Fluid*Specific Heat Capacity of Cold Fluid*(Inlet Temperature of Cold Fluid-Outlet Temperature of Cold Fluid)
  • Heat=Mass of hot fluid*Specific Heat Capacity of Hot Fluid*(Inlet Temperature of Hot Fluid-Outlet Temperature of Hot Fluid)
  • Heat=Number of Moles*Molar Specific Heat Capacity at Constant Volume*Temperature Difference
  • Heat=[R]*Temperature of Gas*ln(Initial Pressure of System/Final Pressure of System)
  • Heat=[R]*Temperature of Gas*ln(Final Volume of System/Initial Volume of System)
  • Heat=(Thermal Conductivity*2*pi*(outer radius-inner radius)*Temperature Difference*length of cylinder)/((ln(outer radius/inner radius))*(outer radius-inner radius))
  • Heat=[Stefan-BoltZ]*Body Surface Area*Geometric View Factor*(Temperature of surface 1^4-Temperature of surface 2^4)
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