Hallo everyone!
I would like someone to explain me/remind me why the definition of isentropic efficiency for the turbine and the compressor is different.
Please see the attached document.
Thank you in advance!
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Posted 15 February 2020 - 07:24 PM
Hallo everyone!
I would like someone to explain me/remind me why the definition of isentropic efficiency for the turbine and the compressor is different.
Please see the attached document.
Thank you in advance!
Posted 16 February 2020 - 03:44 AM
Hi,
Consider this resource to support your query : http://processengine...damentals.html#
note : let you use your favorite search engine .
It's also good to use a H-S diagram to visualize the work !
Good luck
Breizh
Edited by breizh, 16 February 2020 - 06:09 AM.
Posted 16 February 2020 - 03:18 PM
Thank you so much for the valuable documents!!!
The answer is hidden in heat engine and heat pump.
Am I right?
Posted 18 February 2020 - 02:00 AM
hi ,
You need to perform a heat balance for 2 conditions : isentropic and real .
1= initial state
2 = final state
m*(h2-h1) = W+Q with Q# 0 adiabatic
W :work
Q :heat
m : mass flow rate kg/s
hi :specific enthalpy
Compression : h2 isentropic is smaller than h2 real ; RC = (h2 is-h1)/(h2 real -h1) <1
turbine means expansion : h2 real is bigger than h2 isentropic ; RD = -Wreal /-W is =( h1-h2real )/(h1-h2is) <1
Again use a diagram H-S where you plot h1, h2 isentropic and h2 real at P1 and P2 .
https://thermodynami...and-compressor/
My view
Breizh
Edited by breizh, 19 February 2020 - 02:17 AM.
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