-
Notifications
You must be signed in to change notification settings - Fork 1
/
Copy pathregenCEA1.out
206 lines (152 loc) · 8.18 KB
/
regenCEA1.out
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
*******************************************************************************
NASA-GLENN CHEMICAL EQUILIBRIUM PROGRAM CEA2, MAY 21, 2004
BY BONNIE MCBRIDE AND SANFORD GORDON
REFS: NASA RP-1311, PART I, 1994 AND NASA RP-1311, PART II, 1996
*******************************************************************************
problem rocket fr
p(bar) = 17.2369
o/f = 1.2
sup = 1
reac
fuel = C3H8O,2propanol t(K) = 293.150
ox = O2(L) t(K) = 90.170
outp trans
end
OPTIONS: TP=F HP=F SP=F TV=F UV=F SV=F DETN=F SHOCK=F REFL=F INCD=F
RKT=T FROZ=T EQL=F IONS=F SIUNIT=T DEBUGF=F SHKDBG=F DETDBG=F TRNSPT=T
TRACE= 0.00E+00 S/R= 0.000000E+00 H/R= 0.000000E+00 U/R= 0.000000E+00
Pc,BAR = 17.236900
Pc/P =
SUBSONIC AREA RATIOS =
SUPERSONIC AREA RATIOS = 1.0000
NFZ= 1 Mdot/Ac= 0.000000E+00 Ac/At= 0.000000E+00
WARNING!! AMOUNT MISSING FOR REACTANT 1.
PROGRAM SETS WEIGHT PERCENT = 100. (REACT)
WARNING!! AMOUNT MISSING FOR REACTANT 2.
PROGRAM SETS WEIGHT PERCENT = 100. (REACT)
REACTANT WT.FRAC (ENERGY/R),K TEMP,K DENSITY
EXPLODED FORMULA
F: C3H8O,2propanol 1.000000 -0.328516E+05 293.15 0.0000
C 3.00000 H 8.00000 O 1.00000
O: O2(L) 1.000000 -0.156101E+04 90.17 0.0000
O 2.00000
SPECIES BEING CONSIDERED IN THIS SYSTEM
(CONDENSED PHASE MAY HAVE NAME LISTED SEVERAL TIMES)
LAST thermo.inp UPDATE: 9/09/04
g 7/97 *C tpis79 *CH g 4/02 CH2
g 4/02 CH3 g11/00 CH2OH g 7/00 CH3O
g 8/99 CH4 g 7/00 CH3OH srd 01 CH3OOH
tpis79 *CO g 9/99 *CO2 tpis91 COOH
tpis91 *C2 g 6/01 C2H g 1/91 C2H2,acetylene
g 5/01 C2H2,vinylidene g 4/02 CH2CO,ketene g 3/02 O(CH)2O
srd 01 HO(CO)2OH g 7/01 C2H3,vinyl g 6/96 CH3CO,acetyl
g 1/00 C2H4 g 8/88 C2H4O,ethylen-o g 8/88 CH3CHO,ethanal
g 6/00 CH3COOH srd 01 OHCH2COOH g 7/00 C2H5
g 7/00 C2H6 g 8/88 C2H5OH g 7/00 CH3OCH3
srd 01 CH3O2CH3 g 8/00 C2O tpis79 *C3
n 4/98 C3H3,1-propynl n 4/98 C3H3,2-propynl g 2/00 C3H4,allene
g 1/00 C3H4,propyne g 5/90 C3H4,cyclo- g 3/01 C3H5,allyl
g 2/00 C3H6,propylene g 1/00 C3H6,cyclo- g 6/01 C3H6O,propylox
g 6/97 C3H6O,acetone g 1/02 C3H6O,propanal g 7/01 C3H7,n-propyl
g 9/85 C3H7,i-propyl g 2/00 C3H8 g 2/00 C3H8O,1propanol
g 2/00 C3H8O,2propanol g 7/88 C3O2 g tpis *C4
g 7/01 C4H2,butadiyne g 8/00 C4H4,1,3-cyclo- n10/92 C4H6,butadiene
n10/93 C4H6,1butyne n10/93 C4H6,2butyne g 8/00 C4H6,cyclo-
n 4/88 C4H8,1-butene n 4/88 C4H8,cis2-buten n 4/88 C4H8,tr2-butene
n 4/88 C4H8,isobutene g 8/00 C4H8,cyclo- g10/00 (CH3COOH)2
n10/84 C4H9,n-butyl n10/84 C4H9,i-butyl g 1/93 C4H9,s-butyl
g 1/93 C4H9,t-butyl g12/00 C4H10,n-butane g 8/00 C4H10,isobutane
g 8/00 *C5 g 5/90 C5H6,1,3cyclo- g 1/93 C5H8,cyclo-
n 4/87 C5H10,1-pentene g 2/01 C5H10,cyclo- n10/84 C5H11,pentyl
g 1/93 C5H11,t-pentyl n10/85 C5H12,n-pentane n10/85 C5H12,i-pentane
n10/85 CH3C(CH3)2CH3 g 2/93 C6H2 g11/00 C6H5,phenyl
g 8/00 C6H5O,phenoxy g 8/00 C6H6 g 8/00 C6H5OH,phenol
g 1/93 C6H10,cyclo- n 4/87 C6H12,1-hexene g 6/90 C6H12,cyclo-
n10/83 C6H13,n-hexyl g 6/01 C6H14,n-hexane g 7/01 C7H7,benzyl
g 1/93 C7H8 g12/00 C7H8O,cresol-mx n 4/87 C7H14,1-heptene
n10/83 C7H15,n-heptyl n10/85 C7H16,n-heptane n10/85 C7H16,2-methylh
n 4/89 C8H8,styrene n10/86 C8H10,ethylbenz n 4/87 C8H16,1-octene
n10/83 C8H17,n-octyl n 4/85 C8H18,n-octane n 4/85 C8H18,isooctane
n10/83 C9H19,n-nonyl g 3/01 C10H8,naphthale n10/83 C10H21,n-decyl
g 8/00 C12H9,o-bipheny g 8/00 C12H10,biphenyl g 6/97 *H
g 1/01 HCO g 6/01 HCCO g 4/02 HO2
tpis78 *H2 g 5/01 HCHO,formaldehy g 6/01 HCOOH
g 8/89 H2O g 6/99 H2O2 g 6/01 (HCOOH)2
g 5/97 *O g 4/02 *OH tpis89 *O2
g 8/01 O3 n 4/83 C(gr) n 4/83 C(gr)
n 4/83 C(gr) g11/99 H2O(cr) g 8/01 H2O(L)
g 8/01 H2O(L)
SPECIES WITH TRANSPORT PROPERTIES
PURE SPECIES
C CH4 CH3OH CO
CO2 C2H2,acetylene
C2H4 C2H6 C2H5OH H
H2 H2O
O OH O2
BINARY INTERACTIONS
C O
CH4 O2
CO CO2
CO O2
CO2 H2
CO2 H2O
CO2 O2
H H2
H O
H2 H2O
H2 O2
H2O O2
O O2
O/F = 1.200000
EFFECTIVE FUEL EFFECTIVE OXIDANT MIXTURE
ENTHALPY h(2)/R h(1)/R h0/R
(KG-MOL)(K)/KG -0.54666124E+03 -0.48783267E+02 -0.27509143E+03
KG-FORM.WT./KG bi(2) bi(1) b0i
*C 0.49920942E-01 0.00000000E+00 0.22691337E-01
*H 0.13312251E+00 0.00000000E+00 0.60510233E-01
*O 0.16640314E-01 0.62502344E-01 0.41655967E-01
POINT ITN T C H O
1 20 2667.580 -12.669 -9.447 -19.194
THEORETICAL ROCKET PERFORMANCE ASSUMING FROZEN COMPOSITION
Pin = 250.0 PSIA
CASE =
REACTANT WT FRACTION ENERGY TEMP
(SEE NOTE) KJ/KG-MOL K
FUEL C3H8O,2propanol 1.0000000 -273145.105 293.150
OXIDANT O2(L) 1.0000000 -12979.000 90.170
O/F= 1.20000 %FUEL= 45.454545 R,EQ.RATIO= 1.815773 PHI,EQ.RATIO= 1.996763
CHAMBER THROAT EXIT
Pinf/P 1.0000 1.7965 1.7965
P, BAR 17.237 9.5946 9.5946
T, K 2667.58 2383.62 2383.62
RHO, KG/CU M 1.4618 0 9.1060-1 9.1060-1
H, KJ/KG -2287.25 -2940.72 -2940.72
U, KJ/KG -3466.43 -3994.38 -3994.38
G, KJ/KG -36788.9 -33769.8 -33769.8
S, KJ/(KG)(K) 12.9337 12.9337 12.9337
M, (1/n) 18.809 18.809 18.809
Cp, KJ/(KG)(K) 2.3203 2.2810 2.2810
GAMMAs 1.2353 1.2404 1.2404
SON VEL,M/SEC 1206.9 1143.2 1143.2
MACH NUMBER 0.000 1.000 1.000
TRANSPORT PROPERTIES (GASES ONLY)
CONDUCTIVITY IN UNITS OF MILLIWATTS/(CM)(K)
VISC,MILLIPOISE 0.84660 0.78032 0.78032
WITH FROZEN REACTIONS
Cp, KJ/(KG)(K) 2.3203 2.2810 2.2810
CONDUCTIVITY 3.3457 3.0140 3.0140
PRANDTL NUMBER 0.5871 0.5905 0.5905
PERFORMANCE PARAMETERS
Ae/At 1.00000 1.0000
CSTAR, M/SEC 1655.8 1655.8
CF 0.6904 0.6904
Ivac, M/SEC 2064.9 2064.9
Isp, M/SEC 1143.2 1143.2
MOLE FRACTIONS
*CO 0.36664 *CO2 0.06017 *H 0.00630
*H2 0.27036 H2O 0.29464 *O 0.00003
*OH 0.00186 *O2 0.00001
* THERMODYNAMIC PROPERTIES FITTED TO 20000.K
PRODUCTS WHICH WERE CONSIDERED BUT WHOSE MOLE FRACTIONS
WERE LESS THAN 5.000000E-06 FOR ALL ASSIGNED CONDITIONS
NOTE. WEIGHT FRACTION OF FUEL IN TOTAL FUELS AND OF OXIDANT IN TOTAL OXIDANTS