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Category > Engineering Posted 18 Jun 2017 My Price 6.00

A gas at upstream conditions (T1,P1) is throttled to a downstream pressure of 1.2 bar.

A gas at upstream conditions (T1,P1) is throttled to a downstream pressure of 1.2 bar. Use the RedlicNKwong equation to estimate the downstream temperature and AS of the gas for one of the following:

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Alpha Geek
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Status NEW Posted 18 Jun 2017 06:06 AM My Price 6.00

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file 1497768287-Answer.docx preview (404 words )
P-----------art----------- a ----------- R-----------edl-----------ich----------- an-----------d K-----------won-----------g r-----------ela-----------tio-----------n ------------ P -----------= R-----------.T -----------/Vm----------- -b----------- - -----------a /-----------T ^-----------1/2----------- *V-----------m (----------- Vm----------- +b----------- ) -----------a =----------- 0.-----------427-----------8 *-----------R^2-----------*Tc----------- ^5-----------/2 -----------/Pc----------- b -----------=0.-----------086-----------7 *-----------R*T-----------c /-----------Pc -----------now----------- , -----------P/P-----------c Z----------- = -----------Vm -----------/ V-----------m- -----------b ------------ a -----------/RT----------- * -----------( V-----------m +-----------b )----------- * -----------T^1-----------/2 -----------cri-----------tic-----------al -----------pro-----------per-----------tie-----------s o-----------f g-----------ase-----------s G-----------ASE-----------S T-----------1 P-----------1 P-----------2 P-----------c T-----------c V-----------c V-----------m k----------- ba-----------r b-----------ar -----------bar----------- k -----------l /-----------mol----------- CO-----------2 3-----------50 -----------80 -----------1.2----------- 73-----------.8 -----------304-----------.18----------- 0.-----------092----------- C2-----------H4 -----------350----------- 60----------- 1.-----------2 5-----------0.5----------- 26-----------8.4-----------2 0----------- .1-----------311----------- N2----------- 25-----------0 6-----------0 1-----------.2 -----------34 -----------126-----------.19----------- 0.-----------113-----------6 C-----------3H8----------- 40-----------0 2-----------0 1-----------.2 -----------43.-----------3 3-----------69.-----------15 -----------1.0-----------23 -----------*10----------- ^------------4 p-----------art----------- a -----------for----------- C0-----------2 g-----------as -----------a =----------- 0.-----------424-----------8
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