thank u so much dear yogi_process
you right, but i want to consider off design conditions.
turbo-compressors designed in ISO condition, but work on different conditions.
as u know, by decreasing inlet air T, net obtained power will be increased.
my results are good in "design condition": stack T, net Power, compressor load and so on
but i can not investigate off design conditions.
by the way, Standard/Actual Volumetric flow means specific mass flow @ design condition, Ok?
now, if T decreases, mass flow increased and we can obtain more work (Mdot*deltaP) from the same flow. isn't it?
if i'm wrong, please tell me how can i reproduce this figure?
[link Point to another website Only the registered members can access]
Figure 20-15. Correction factor for power as a function of inlet ambient air
temperature.
Gas turbine engineering handbook / Meherwan P. Boyce. – 3rd ed, p 750.
as i said, as i said, i think it is due to mass conservation in the material stream that is entered to the air compressor. (when T increases, mass density will be decreased and actual flow will be increased thus mass flow will conserved and vice verse)
P.M:
when i adjust fuel consumption (mass flow) to the mass density of inlet air, results seem good! but this is not a straight forward method!
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