Heat Added in Gas Turbine Combustion Solution

STEP 0: Pre-Calculation Summary
Formula Used
Heat Added = Enthalpy after Combustion-Enthalpy before Combustion
Q = h3-h2
This formula uses 3 Variables
Variables Used
Heat Added - (Measured in Joule) - Heat added is the amount of heat added to a system.
Enthalpy after Combustion - (Measured in Joule) - Enthalpy after combustion is the increase in the enthalpy of fluid after adding heat.
Enthalpy before Combustion - (Measured in Joule) - Enthalpy before Combustion is the amount of energy contained by fluid after compression.
STEP 1: Convert Input(s) to Base Unit
Enthalpy after Combustion: 1700 Kilojoule --> 1700000 Joule (Check conversion ​here)
Enthalpy before Combustion: 310 Kilojoule --> 310000 Joule (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Q = h3-h2 --> 1700000-310000
Evaluating ... ...
Q = 1390000
STEP 3: Convert Result to Output's Unit
1390000 Joule -->1390 Kilojoule (Check conversion ​here)
FINAL ANSWER
1390 Kilojoule <-- Heat Added
(Calculation completed in 00.004 seconds)

Credits

Creator Image
Created by Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!
Verifier Image
Verified by Sagar S Kulkarni
Dayananda Sagar College of Engineering (DSCE), Bengaluru
Sagar S Kulkarni has verified this Calculator and 200+ more calculators!

Combustion Chamber Calculators

Heat Added in Gas Turbine Combustion given Temperature
​ LaTeX ​ Go Heat Added = Specific Heat Capacity at Constant Pressure*(Exit Temperature-Inlet Temperature)
Heat Added in Gas Turbine Combustion
​ LaTeX ​ Go Heat Added = Enthalpy after Combustion-Enthalpy before Combustion

Heat Added in Gas Turbine Combustion Formula

​LaTeX ​Go
Heat Added = Enthalpy after Combustion-Enthalpy before Combustion
Q = h3-h2

What is heat?

Heat is a form of energy, which flows from hotter body to colder body as a result of temperature difference between two bodies.

How to Calculate Heat Added in Gas Turbine Combustion?

Heat Added in Gas Turbine Combustion calculator uses Heat Added = Enthalpy after Combustion-Enthalpy before Combustion to calculate the Heat Added, Heat Added in Gas Turbine Combustion formula is defined as the difference between enthalpy after combustion and enthalpy before combustion. Heat Added is denoted by Q symbol.

How to calculate Heat Added in Gas Turbine Combustion using this online calculator? To use this online calculator for Heat Added in Gas Turbine Combustion, enter Enthalpy after Combustion (h3) & Enthalpy before Combustion (h2) and hit the calculate button. Here is how the Heat Added in Gas Turbine Combustion calculation can be explained with given input values -> 1.39 = 1700000-310000.

FAQ

What is Heat Added in Gas Turbine Combustion?
Heat Added in Gas Turbine Combustion formula is defined as the difference between enthalpy after combustion and enthalpy before combustion and is represented as Q = h3-h2 or Heat Added = Enthalpy after Combustion-Enthalpy before Combustion. Enthalpy after combustion is the increase in the enthalpy of fluid after adding heat & Enthalpy before Combustion is the amount of energy contained by fluid after compression.
How to calculate Heat Added in Gas Turbine Combustion?
Heat Added in Gas Turbine Combustion formula is defined as the difference between enthalpy after combustion and enthalpy before combustion is calculated using Heat Added = Enthalpy after Combustion-Enthalpy before Combustion. To calculate Heat Added in Gas Turbine Combustion, you need Enthalpy after Combustion (h3) & Enthalpy before Combustion (h2). With our tool, you need to enter the respective value for Enthalpy after Combustion & Enthalpy before Combustion 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 Added?
In this formula, Heat Added uses Enthalpy after Combustion & Enthalpy before Combustion. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Heat Added = Specific Heat Capacity at Constant Pressure*(Exit Temperature-Inlet Temperature)
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!