Heat Transfer in Isobaric Process Calculator

✖Number of Moles of Ideal Gas is the amount of gas present in moles. 1 mole of gas weighs as much as its molecular weight.ⓘ Number of Moles of Ideal Gas [n]			+10% -10%
✖Molar Specific Heat Capacity at Constant Pressure, (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 pressure.ⓘ Molar Specific Heat Capacity at Constant Pressure [C_{p molar}]			+10% -10%
✖Temperature Difference is the measure of the hotness or the coldness of an object.ⓘ Temperature Difference [ΔT]			+10% -10%

✖Heat Transferred in Thermodynamic Process is the form of energy that is transferred from the high-temperature system to the low-temperature system.ⓘ Heat Transfer in Isobaric Process [Q]

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Formula

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Heat Transfer in Isobaric Process

Formula

`"Q" = "n"*"C"_{"p molar"}*"ΔT"`

Example

`"146400J"="3mol"*"122J/K*mol"*"400K"`

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Heat Transfer in Isobaric Process Solution

STEP 0: Pre-Calculation Summary

Formula Used

Heat Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference
Q = n*C_{p molar}*ΔT
This formula uses 4 Variables

Variables Used

Heat Transferred in Thermodynamic Process - (Measured in Joule) - Heat Transferred in Thermodynamic Process is the form of energy that is transferred from the high-temperature system to the low-temperature system.
Number of Moles of Ideal Gas - (Measured in Mole) - Number of Moles of Ideal Gas is the amount of gas present in moles. 1 mole of gas weighs as much as its molecular weight.
Molar Specific Heat Capacity at Constant Pressure - (Measured in Joule Per Kelvin Per Mole) - Molar Specific Heat Capacity at Constant Pressure, (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 pressure.
Temperature Difference - (Measured in Kelvin) - Temperature Difference is the measure of the hotness or the coldness of an object.

STEP 1: Convert Input(s) to Base Unit

Number of Moles of Ideal Gas: 3 Mole --> 3 Mole No Conversion Required
Molar Specific Heat Capacity at Constant Pressure: 122 Joule Per Kelvin Per Mole --> 122 Joule Per Kelvin Per Mole No Conversion Required
Temperature Difference: 400 Kelvin --> 400 Kelvin No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

Q = n*C_{p molar}*ΔT --> 3*122*400

Evaluating ... ...

Q = 146400

STEP 3: Convert Result to Output's Unit

146400 Joule --> No Conversion Required

FINAL ANSWER

146400 Joule <-- Heat Transferred in Thermodynamic Process

(Calculation completed in 00.004 seconds)

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Created by Ishan Gupta

Birla Institute of Technology & Science (BITS), Pilani

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< 20 Ideal Gas Calculators

Work Done in Adiabatic Process using Specific Heat Capacity at Constant Pressure and Volume

Go Work done in Thermodynamic Process = (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)

Final Temperature in Adiabatic Process (using pressure)

Go Final Temperature in Adiabatic Process = Initial temperature of Gas*(Final Pressure of System/Initial Pressure of System)^(1-1/(Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume))

Final Temperature in Adiabatic Process (using volume)

Go Final Temperature in Adiabatic Process = Initial temperature of Gas*(Initial Volume of System/Final Volume of System)^((Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume)-1)

Work Done in Isothermal Process (using volume)

Go Work done in Thermodynamic Process = Number of Moles of Ideal Gas* [R]*Temperature of Gas*ln(Final Volume of System/Initial Volume of System)

Heat Transferred in Isothermal Process (using Pressure)

Go Heat Transferred in Thermodynamic Process = [R]*Initial temperature of Gas*ln(Initial Pressure of System/Final Pressure of System)

Heat Transferred in Isothermal Process (using Volume)

Go Heat Transferred in Thermodynamic Process = [R]*Initial temperature of Gas*ln(Final Volume of System/Initial Volume of System)

Work done in Isothermal Process (using Pressure)

Go Work done in Thermodynamic Process = [R]*Temperature of Gas*ln(Initial Pressure of System/Final Pressure of System)

Relative Humidity

Go Relative Humidity = Specific Humidity*Partial Pressure/((0.622+Specific Humidity)*Vapor Pressure of Pure Component A)

Heat Transfer in Isobaric Process

Go Heat Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference

Heat Transfer in Isochoric Process

Go Heat Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Volume*Temperature Difference

Change in Internal Energy of System

Go Change in Internal Energy = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Volume*Temperature Difference

Enthalpy of System

Go System Enthalpy = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference

Ideal Gas Law for Calculating Volume

Go Ideal Gas Law for Calculating Volume = [R]*Temperature of Gas/Total Pressure of Ideal Gas

Ideal Gas Law for Calculating Pressure

Go Ideal Gas Law for calculating Pressure = [R]*(Temperature of Gas)/Total Volume of System

Adiabatic Index

Go Heat Capacity Ratio = Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume

Specific Heat Capacity at Constant Pressure

Go Molar Specific Heat Capacity at Constant Pressure = [R]+Molar Specific Heat Capacity at Constant Volume

Specific Heat Capacity at Constant Volume

Go Molar Specific Heat Capacity at Constant Volume = Molar Specific Heat Capacity at Constant Pressure-[R]

Henry Law Constant using Mole Fraction and Partial Pressure of Gas

Go Henry Law Constant = Partial Pressure/Mole Fraction of Component in Liquid Phase

Mole Fraction of Dissolved Gas using Henry Law

Go Mole Fraction of Component in Liquid Phase = Partial Pressure/Henry Law Constant

Partial Pressure using Henry Law

Go Partial Pressure = Henry Law Constant*Mole Fraction of Component in Liquid Phase

Heat Transfer in Isobaric Process Formula

Heat Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference
Q = n*C_{p molar}*ΔT

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 Isobaric Process?

Heat Transfer in Isobaric Process calculator uses Heat Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference to calculate the Heat Transferred in Thermodynamic Process, Heat Transfer in 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 Transferred in Thermodynamic Process is denoted by Q symbol.

How to calculate Heat Transfer in Isobaric Process using this online calculator? To use this online calculator for Heat Transfer in Isobaric Process, enter Number of Moles of Ideal Gas (n), Molar Specific Heat Capacity at Constant Pressure (C_{p molar}) & Temperature Difference (ΔT) and hit the calculate button. Here is how the Heat Transfer in Isobaric Process calculation can be explained with given input values -> 146400 = 3*122*400.

FAQ

What is Heat Transfer in Isobaric Process?

Heat Transfer in 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*C_{p molar}*ΔT or Heat Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference. Number of Moles of Ideal Gas is the amount of gas present in moles. 1 mole of gas weighs as much as its molecular weight, Molar Specific Heat Capacity at Constant Pressure, (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 pressure & Temperature Difference is the measure of the hotness or the coldness of an object.

How to calculate Heat Transfer in Isobaric Process?

Heat Transfer in 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 Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Pressure*Temperature Difference. To calculate Heat Transfer in Isobaric Process, you need Number of Moles of Ideal Gas (n), Molar Specific Heat Capacity at Constant Pressure (C_{p molar}) & Temperature Difference (ΔT). With our tool, you need to enter the respective value for Number of Moles of Ideal Gas, Molar Specific Heat Capacity at Constant Pressure & Temperature Difference 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 Transferred in Thermodynamic Process?

In this formula, Heat Transferred in Thermodynamic Process uses Number of Moles of Ideal Gas, Molar Specific Heat Capacity at Constant Pressure & Temperature Difference. We can use 3 other way(s) to calculate the same, which is/are as follows -

Heat Transferred in Thermodynamic Process = Number of Moles of Ideal Gas*Molar Specific Heat Capacity at Constant Volume*Temperature Difference
Heat Transferred in Thermodynamic Process = [R]*Initial temperature of Gas*ln(Initial Pressure of System/Final Pressure of System)
Heat Transferred in Thermodynamic Process = [R]*Initial temperature of Gas*ln(Final Volume of System/Initial Volume of System)

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