diff options
author | prashantsinalkar | 2017-10-10 12:38:01 +0530 |
---|---|---|
committer | prashantsinalkar | 2017-10-10 12:38:01 +0530 |
commit | f35ea80659b6a49d1bb2ce1d7d002583f3f40947 (patch) | |
tree | eb72842d800ac1233e9d890e020eac5fd41b0b1b /1472 | |
parent | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (diff) | |
download | Scilab-TBC-Uploads-f35ea80659b6a49d1bb2ce1d7d002583f3f40947.tar.gz Scilab-TBC-Uploads-f35ea80659b6a49d1bb2ce1d7d002583f3f40947.tar.bz2 Scilab-TBC-Uploads-f35ea80659b6a49d1bb2ce1d7d002583f3f40947.zip |
updated the code
Diffstat (limited to '1472')
-rwxr-xr-x | 1472/CH10/EX10.5/10_5.sce | 28 | ||||
-rwxr-xr-x | 1472/CH11/EX11.5.c/11_5c.sce | 45 | ||||
-rwxr-xr-x | 1472/CH16/EX16.2/16_2.sce | 35 | ||||
-rwxr-xr-x | 1472/CH17/EX17.1.b/17_1b.sce | 27 | ||||
-rwxr-xr-x | 1472/CH17/EX17.3.b/17_3b.sce | 65 | ||||
-rwxr-xr-x | 1472/CH21/EX21.3/21_3.sce | 43 | ||||
-rwxr-xr-x | 1472/CH23/EX23.4/23_4.sce | 113 |
7 files changed, 181 insertions, 175 deletions
diff --git a/1472/CH10/EX10.5/10_5.sce b/1472/CH10/EX10.5/10_5.sce index bc0d5d9a7..e0021570e 100755 --- a/1472/CH10/EX10.5/10_5.sce +++ b/1472/CH10/EX10.5/10_5.sce @@ -1,14 +1,14 @@ -clc
-//initialization of varaibles
-x=0.97
-P=100 //psia
-//calculations
-disp("From table 2,")
-hf=298.4
-hfg=888.8
-hx=hf+x*hfg
-hg=1187.2
-hx2=hg-(1-x)*hfg
-//results
-printf("Accurate Enthalpy = %.1f B/lb",hx2)
-printf("\n Enthalpy = %d B/lb")
+clc +//initialization of variables +x=0.97 +P=100 //psia +//calculations +disp("From table 2,") +hf=298.4 +hfg=888.8 +hx=hf+x*hfg +hg=1187.2 +hx2=hg-(1-x)*hfg +//results +printf("Accurate Enthalpy = %.1f B/lb",hx2) +printf("\n Enthalpy = %.1f B/lb", hg)
\ No newline at end of file diff --git a/1472/CH11/EX11.5.c/11_5c.sce b/1472/CH11/EX11.5.c/11_5c.sce index 56beaa1e8..fad2d13c3 100755 --- a/1472/CH11/EX11.5.c/11_5c.sce +++ b/1472/CH11/EX11.5.c/11_5c.sce @@ -1,22 +1,23 @@ -clc
-//initialization of varaibles
-P1=100 //psia
-T1=2000+460 //R
-P2=15 //psia
-g=1.4
-cp=0.276
-cv=0.207
-T2=1520 //R
-//calculations
-h1=634.4
-pr1=407.3
-pr2=pr1*P2/P1
-disp("From table 1,")
-T2=1535 //R
-h2=378.44
-dh=h2-h1
-v2=53.34*T2/(P2*144)
-dv=v2-v1
-//results
-printf("Enthalpy change = %.2f B/lb",dh)
-printf("\n Volume change = %.1f cu ft/lb",dv)
+clc +//initialization of variables +P1=100 //psia +T1=2000+460 //R +P2=15 //psia +g=1.4 +cp=0.276 +cv=0.207 +T2=1520 //R +//calculations +h1=634.4 +pr1=407.3 +pr2=pr1*P2/P1 +disp("From table 1,") +T2=1535 //R +h2=378.44 +dh=h2-h1 +v1=53.34*T1/(P1*144) +v2=53.34*T2/(P2*144) +dv=v2-v1 +//results +printf("Enthalpy change = %.2f B/lb",dh) +printf("\n Volume change = %.1f cu ft/lb",dv)
\ No newline at end of file diff --git a/1472/CH16/EX16.2/16_2.sce b/1472/CH16/EX16.2/16_2.sce index b9336080e..5317d6746 100755 --- a/1472/CH16/EX16.2/16_2.sce +++ b/1472/CH16/EX16.2/16_2.sce @@ -1,17 +1,18 @@ -clc
-//initialization of varaibles
-e=0.75
-Ta=870 //R
-Tc=1075//R
-cp=0.24
-Td=550 //R
-//calculations
-Tadash=e*(Tc-Ta) +Ta
-Tcdash=Tc+Ta-Tadash
-Q1=cp*(Tb-Tadash)
-Q2=cp*(Tcdash-Td)
-Wnet=Q1-Q2
-eta=Wnet/Q1
-//results
-printf("Net work done = %d B/lb",Wnet)
-printf("\n efficiency = %.2f ",eta)
+clc +//initialization of variables +e=0.75 +Ta=870 //R +Tc=1075//R +cp=0.24 +Td=550 //R +Tb=1700; +//calculations +Tadash=e*(Tc-Ta) +Ta +Tcdash=Tc+Ta-Tadash +Q1=cp*(Tb-Tadash) +Q2=cp*(Tcdash-Td) +Wnet=Q1-Q2 +eta=Wnet/Q1 +//results +printf("Net work done = %d B/lb",Wnet) +printf("\n efficiency = %.2f ",eta)
\ No newline at end of file diff --git a/1472/CH17/EX17.1.b/17_1b.sce b/1472/CH17/EX17.1.b/17_1b.sce index 0a7bb1974..d97b02f13 100755 --- a/1472/CH17/EX17.1.b/17_1b.sce +++ b/1472/CH17/EX17.1.b/17_1b.sce @@ -1,13 +1,14 @@ -clc
-//initialization of varaibles
-k=1.3
-P=100 //psia
-//calculations
-Pratio=(2/(k+1))^(k/(k-1))
-Pt=Pratio*P
-disp("From table 3,")
-ht=1221.5 //B/lb
-vt=8.841 //cu ft/lb
-at=w*vt/1700
-//results
-printf("Throat area = %.4f sq ft",at)
+clc +//initialization of variables +w = 1; +k=1.3 +P=100 //psia +//calculations +Pratio=(2/(k+1))^(k/(k-1)) +Pt=Pratio*P +disp("From table 3,") +ht=1221.5 //B/lb +vt=8.841 //cu ft/lb +at=w*vt/1700 +//results +printf("Throat area = %.4f sq ft",at)
\ No newline at end of file diff --git a/1472/CH17/EX17.3.b/17_3b.sce b/1472/CH17/EX17.3.b/17_3b.sce index 00e93490c..eaa6adbba 100755 --- a/1472/CH17/EX17.3.b/17_3b.sce +++ b/1472/CH17/EX17.3.b/17_3b.sce @@ -1,32 +1,33 @@ -clc
-//initialization of varaibles
-h0=191.81 //B/lb
-Pr0=5.526
-w=1 //lb/sec
-Pratio=0.53
-k=1.4
-T0=800 //R
-cp=0.24
-P0=150 //psia
-P2=15 //psia
-//calculations
-Prt=Pratio*Pr0
-disp("From keenan and kaye steam tables,")
-Pr=2.929
-Tts=668 //R
-hts=159.9 //B/lb
-Vts=sqrt(2*32.2*778*(h0-hts))
-vts=53.34*Tts/(Pt*144)
-at=w*vts/(Vts)
-Pr2=P2*Pr0/P0
-T2s=415 //R
-h2s=99.13 //B/lb
-h2=110.25 //B/lb
-T2=462 //R
-V2=sqrt(2*32.2*778*(h0-h2))
-v2=53.34*T2/(144*P2)
-a2=w*v2/V2
-//results
-printf("Exit velocity = %d fps",Vts)
-printf("\n Throat area = %.5f ft^2",at)
-printf("\n Exit area = %.5f ft^2",a2)
+clc +//initialization of variables +h0=191.81 //B/lb +Pr0=5.526 +w=1 //lb/sec +Pratio=0.53 +k=1.4 +T0=800 //R +cp=0.24 +P0=150 //psia +P2=15 //psia +Pt=79.5; +//calculations +Prt=Pratio*Pr0 +disp("From keenan and kaye steam tables,") +Pr=2.929 +Tts=668 //R +hts=159.9 //B/lb +Vts=sqrt(2*32.2*778*(h0-hts)) +vts=53.34*Tts/(Pt*144) +at=w*vts/(Vts) +Pr2=P2*Pr0/P0 +T2s=415 //R +h2s=99.13 //B/lb +h2=110.25 //B/lb +T2=462 //R +V2=sqrt(2*32.2*778*(h0-h2)) +v2=53.34*T2/(144*P2) +a2=w*v2/V2 +//results +printf("Exit velocity = %d fps",Vts) +printf("\n Throat area = %.5f ft^2",at) +printf("\n Exit area = %.5f ft^2",a2)
\ No newline at end of file diff --git a/1472/CH21/EX21.3/21_3.sce b/1472/CH21/EX21.3/21_3.sce index 0cdb4760a..6e12126cb 100755 --- a/1472/CH21/EX21.3/21_3.sce +++ b/1472/CH21/EX21.3/21_3.sce @@ -1,21 +1,22 @@ -clc
-//initialization of varaibles
-R=53.34
-T1=540 //R
-n=1.4
-g=n
-n2=1.3
-P2=90 //psia
-P1=15 //psia
-cv=0.171
-eta=0.95
-//calculations
-pv=R*T1
-Wk=n*R*T1*((P2/P1)^((g-1)/g) -1) /(n-1)
-Wn=n2*R*T1*((P2/P1)^((n2-1)/n2) -1) /(n2-1)
-Wt=R*T1*log(P2/P1)
-Wx=-Wk/eta
-dh=cp*T1*(1.52 - 1)
-Q=dh+Wx/778
-//results
-printf("Heat transferred = %.1f B/lb",Q)
+clc +//initialization of variables +R=53.34 +T1=540 //R +n=1.4 +g=n +n2=1.3 +P2=90 //psia +P1=15 //psia +cv=0.171 +cp=0.24; +eta=0.95 +//calculations +pv=R*T1 +Wk=n*R*T1*((P2/P1)^((g-1)/g) -1) /(n-1) +Wn=n2*R*T1*((P2/P1)^((n2-1)/n2) -1) /(n2-1) +Wt=R*T1*log(P2/P1) +Wx=-Wk/eta +dh=cp*T1*(1.52 - 1) +Q=dh+Wx/778 +//results +printf("Heat transferred = %.1f B/lb",Q)
\ No newline at end of file diff --git a/1472/CH23/EX23.4/23_4.sce b/1472/CH23/EX23.4/23_4.sce index ad9a56c1e..1345b351c 100755 --- a/1472/CH23/EX23.4/23_4.sce +++ b/1472/CH23/EX23.4/23_4.sce @@ -1,56 +1,57 @@ -clc
-//initialization of varaibles
-V1=587 //fps
-etaD=0.9
-etaC=0.8
-h1=114.69
-P1=10 //psia
-P6=P1
-dhB=-19100 //B/lb
-T1=480 //R
-//calculations
-h2s=etaD*V1^2 /(778*2*32.2) +h1
-disp("From tables,")
-Pr2s=1.104
-Pr1=0.9182
-P2=P1*Pr2s/Pr1
-h2=h1+(h2s-h1)/etaD
-T2=509 //R
-Pr2=1.127
-Pr3s=Pr2*P3/P2
-Pr3s=6.76
-h3s=203.2
-h3=(h3s-h2)/etaC +h2
-T3=930 //R
-P3=6*P2
-T4=2160 //R
-h4=549.35
-Pr4=238
-h4B=126.66
-dh4=422.7
-h3B=h4B
-dh3=h3-h3B
-cp=0.5
-Ta=480 //R
-Tb=530 //R
-dhf=cp*(Tb-Ta)
-wratio=(-dh4+dh3)/(dh4+dhf+dhB)
-h5s=425.3
-Pr5s=93.1
-P5=27.6
-T5=1801 //R
-Pr5=114.28
-Pr6s=Pr5*P6/P5
-h5=450
-h6=351
-V6=sqrt(2*32.2*778*(h5-h6))
-SI=((1+wratio)*V6 -V1)/(32.2)
-v1=53.34*T1/(P1*144)
-wa=V1/v1
-thrust = wa*SI
-SC=wa*0.0174*3600/1840
-eff=2545/(SC*-dhB)
-//results
-printf("Specific impulse = %.1f lb/lb per sec of air",SI)
-printf("\n Thrust = %d lb",thrust)
-printf("\n Efficiency = %.3f",eff)
+clc +//initialization of variables +V1=587 //fps +etaD=0.9 +etaC=0.8 +h1=114.69 +P1=10 //psia +P3=626; +P6=P1 +dhB=-19100 //B/lb +T1=480 //R +//calculations +h2s=etaD*V1^2 /(778*2*32.2) +h1 +disp("From tables,") +Pr2s=1.104 +Pr1=0.9182 +P2=P1*Pr2s/Pr1 +h2=h1+(h2s-h1)/etaD +T2=509 //R +Pr2=1.127 +Pr3s=Pr2*P3/P2 +Pr3s=6.76 +h3s=203.2 +h3=(h3s-h2)/etaC +h2 +T3=930 //R +P3=6*P2 +T4=2160 //R +h4=549.35 +Pr4=238 +h4B=126.66 +dh4=422.7 +h3B=h4B +dh3=h3-h3B +cp=0.5 +Ta=480 //R +Tb=530 //R +dhf=cp*(Tb-Ta) +wratio=(-dh4+dh3)/(dh4+dhf+dhB) +h5s=425.3 +Pr5s=93.1 +P5=27.6 +T5=1801 //R +Pr5=114.28 +Pr6s=Pr5*P6/P5 +h5=450 +h6=351 +V6=sqrt(2*32.2*778*(h5-h6)) +SI=((1+wratio)*V6 -V1)/(32.2) +v1=53.34*T1/(P1*144) +wa=V1/v1 +thrust = wa*SI +SC=wa*0.0174*3600/1840 +eff=2545/(SC*-dhB) +//results +printf("Specific impulse = %.1f lb/lb per sec of air",SI) +printf("\n Thrust = %d lb",thrust) +printf("\n Efficiency = %.3f",eff)
\ No newline at end of file |