FormulaDen.com
Physics
Chemistry
Math
Chemical Engineering
Civil
Electrical
Electronics
Electronics and Instrumentation
Materials Science
Mechanical
Production Engineering
Financial
Health
You are here
-
Home
»
Physics
»
Aerospace
»
Propulsion
Heat Capacity Ratio in Components of Gas Turbine Formulas
The Heat Capacity Ratio also known as the adiabatic index is the ratio of specific heats i.e. the ratio of the heat capacity at constant pressure to heat capacity at constant volume. And is denoted by γ.
Components of Gas Turbine formulas that make use of Heat Capacity Ratio
f
x
Minimum Temperature Ratio
Go
FAQ
What is the Heat Capacity Ratio?
The Heat Capacity Ratio also known as the adiabatic index is the ratio of specific heats i.e. the ratio of the heat capacity at constant pressure to heat capacity at constant volume.
Can the Heat Capacity Ratio be negative?
{YesorNo}, the Heat Capacity Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!