Help with thermodynamics problem

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Homework Help Overview

The discussion revolves around a thermodynamics problem involving the isentropic compression of air using a two-stage compressor. The goal is to determine the optimal intermediate pressure that minimizes total compression work when compressing air from 1 atm to 25 atm.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning, Problem interpretation

Approaches and Questions Raised

  • Participants discuss the equation for the intermediate pressure, questioning its derivation and the assumptions involved, such as whether air can be treated as an ideal gas. There are attempts to derive the total work for each compression stage and explore conditions for minimizing work.

Discussion Status

The discussion is ongoing, with participants actively seeking clarification on the derivation of the relevant equations and exploring different approaches to the problem. Some guidance has been offered regarding the use of adiabatic conditions and the relationship between volumes in the two stages of compression.

Contextual Notes

Participants are considering the implications of adiabatic processes and the need to remove heat between compression stages. There is also mention of constraints related to the mathematical expressions for work and the conditions under which they apply.

Deathcrush
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Homework Statement


Hi I would like you guys to help me with this problem

Air is to be compressed steadily and isentropically from 1 atm to 25 atm by a two-stage compressor. To minimize the total compression work, the intermediate pressure between the two stages must be
(a) 3 atm (b) 5 atm (c) 8 atm (d) 10 atm (e) 13 atm

Homework Equations



(a) 3 atm (b) 5 atm (c) 8 atm (d) 10 atm (e) 13 atm

P=sqrt(P1*P2)

The Attempt at a Solution



I found that this pressure can be calculated with the square root of the product of those two pressures, however, i want to know where that equation comes from

thanks!
 
Last edited:
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cmon, help me, please, how do you obtain that equation?
 
Deathcrush said:

Homework Statement


Hi I would like you guys to help me with this problem

Air is to be compressed steadily and isentropically from 1 atm to 25 atm by a two-stage compressor. To minimize the total compression work, the intermediate pressure between the two stages must be
(a) 3 atm (b) 5 atm (c) 8 atm (d) 10 atm (e) 13 atm

Homework Equations



(a) 3 atm (b) 5 atm (c) 8 atm (d) 10 atm (e) 13 atm

P=sqrt(P1*P2)
!
If there is any savings of work by doing it in two stages, the heat from the first compression has to be removed. So compress it to 1/5 of original volume (adiabatic), remove the heat and then adiabatically compress it further to 1/5 of this compressed state.

You should be able to show that if you do it any other way (eg. compress 1/2 then 1/12.5, or vice versa) you will end up doing more work. Write out the mathematical expression for work for the first compression to V1 + work for the second compression to Vf. You have to use the adiabatic condition (T and V) for each compression with a reduction in temperature to initial temperature after the first compression. When is the work a minimum?

AM
 
yeah, well, what i am interested in , is in finding how can I get that equation listed above, I had thought in deriving the equation for the sum of work in each phase, and finding the minimum value, however i can't set the whole thing to get that equation. Can I consider the air as an ideal gas? or how else can I get an equation P to integrate
 
Deathcrush said:
yeah, well, what i am interested in , is in finding how can I get that equation listed above, I had thought in deriving the equation for the sum of work in each phase, and finding the minimum value, however i can't set the whole thing to get that equation. Can I consider the air as an ideal gas? or how else can I get an equation P to integrate
Use the adiabatic condition for the first stage from V0 to V1:

[tex]T_0V_0^{(\gamma-1)} = T_1V_1^{(\gamma-1)}[/tex]

Since it is adiabatic, the work done is equal to the change in internal energy: [itex]W = nC_v\Delta T[/itex]

Do the same for the second stage. Then show that the minimum value for total Work is when V2/V1 = V1/V0 (ie. [itex]V_1 = \sqrt{V_2V_0}[/itex]).

AM
 
I think I'm getting it, I would thank you if you could recommend me some reading about this
 
Last edited:

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