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
Actual Temperature at Compressor Exit in Components of Gas Turbine Formulas
Actual Temperature at Compressor Exit is the temperature of the gases exiting the compressor considering the losses throughout the compression process. And is denoted by T
2,actual
. Actual Temperature at Compressor Exit is usually measured using the Kelvin for Temperature. Note that the value of Actual Temperature at Compressor Exit is always positive.
Components of Gas Turbine formulas that make use of Actual Temperature at Compressor Exit
f
x
Efficiency of compressor in actual gas turbine cycle
Go
FAQ
What is the Actual Temperature at Compressor Exit?
Actual Temperature at Compressor Exit is the temperature of the gases exiting the compressor considering the losses throughout the compression process. Actual Temperature at Compressor Exit is usually measured using the Kelvin for Temperature. Note that the value of Actual Temperature at Compressor Exit is always positive.
Can the Actual Temperature at Compressor Exit be negative?
No, the Actual Temperature at Compressor Exit, measured in Temperature cannot be negative.
What unit is used to measure Actual Temperature at Compressor Exit?
Actual Temperature at Compressor Exit is usually measured using the Kelvin[K] for Temperature. Celsius[K], Fahrenheit[K], Rankine[K] are the few other units in which Actual Temperature at Compressor Exit can be measured.
Let Others Know
✖
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!