Notes

T2T1=(rpc)(?-1)?.nc

rpg=1-?11-?2(rpc)
f=cpgt3-cpat2cv-cpa t2
afr=(1-f)f

exca=(afr-17.24)17.24

t4=t3(rpg)(?-1)nt?

ws=cpg(t4-t5)(ha-hf)

t6=t4-ws(ha-he)cpg

xbs=(sa-0.1059)8,869

hbs=29.30+2484.9(xbs)

wst=ms(ha-hbs)ntst
mg=(ms/ws);
wa=(1-f)mg;
wgt= mgcpg(t3-t4)- wacpa(t2-t1)
wnet= wst + wgt;
wf= f.mg; // mass flow ordinate of fuel

nst=(ha-hbs)ntst(ha-he)ntst

no=wnetwf.cv

ntgt=wgtwf.cv
xl=mg.cpg(t6-t1)wf.cv

no1=nst+ntgt-nst.ntgt-(ntgt.xl)

ra=cpa(?-1)?

ic=wat1[cpalog?(rpc)?-1?.nc-ra.logrpc]

rg=cpg.(n-1)n

igt=mg.t1[cpg.log1rpgn-1ntn-rg.log(1rpg)]

se=2.046

se=2.



046; // constant
ihrsg= t1* ((ms*(sa-se)) + (mg*((cpg*log((t6/t4)))-(rg*log(1/(1+b2))))));
// Steam Turbine
hb= ha - (ntst*(ha-hbs));
xb=(hb-29.30)/2484.9;
sb=0.1059+ (xb*8.869);
ist=ms*(sb-sa)*t1;
// stupefy loss
iexh= mg*cpg*((t6-t1)-(t1*log((t6/t1))));
// combustor
sp3=mg*cpg*log((t3/t1))-mg*rg*log((rpc*(1-b1)));
sr2=mg*cpg*(log(pow(rpc,pow1)))-wa*ra*log(rpc);
//p,r,a & f represent product,reactant, air,fuel
//for ch4
sy=1.0401+(0.1729*4*1)/(1*12);
ho=wf*cv;
go=sy*ho;
so=go-ho;
icomb= t1*(sp3-sr2)+so;If you want to get a total essay, order it on our website: Orderessay



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