- Page 1: NISTIR 6659Thermodynamic, Transport
- Page 7 and 8: Accomplishments and New Findings:Th
- Page 9 and 10: 14 5.291 S 26.3 H 1,2,4-trimethyl b
- Page 11 and 12: decane3-methyldecanetetradecane1315
- Page 13 and 14: external diameter, 0.18 cm internal
- Page 15 and 16: The half-life, t 0.5 , of a decompo
- Page 17 and 18: The thermally stressed liquid phase
- Page 19 and 20: -7-9ln k-11-131.35 1.40 1.45 1.50 1
- Page 21 and 22: 0.01 min. Although we did not attem
- Page 23 and 24: -8-10ln k-12-14-161.35 1.40 1.45 1.
- Page 25 and 26: 270.00 25.004 805.91 390.00 25.009
- Page 27 and 28: MethylcyclohexaneDensity [kg/m3]820
- Page 29 and 30: 350.00 4.999 753.83 470.00 5.003 65
- Page 31 and 32: Figure 12: A photograph of the visc
- Page 33 and 34: Table 10: Kinematic viscosity of me
- Page 35 and 36: w / m·s -114001350Methylcyclohexan
- Page 37 and 38: Thermal Conductivity of Methyl- and
- Page 39 and 40: 0.120.10 e / W . m -1 K -10.080.060
- Page 41 and 42: data. We have applied this method t
- Page 43 and 44: Figure 19: Schematic diagram of the
- Page 45 and 46: Table 13: Representative distillati
- Page 47 and 48: 255245235Temperature, T k, °C22521
- Page 49 and 50: Figure 22: The relationship of T k
- Page 51 and 52: 250.0240.0230.0T k , o C220.0210.0J
- Page 53 and 54:
The distillate fractions of the thr
- Page 55 and 56:
Table 16c: Jet-A-4658:DistillateVol
- Page 57 and 58:
Figure 25: A plot of the hydrocarbo
- Page 59 and 60:
These two facts are consistent with
- Page 61 and 62:
260Temperature, T k , o C2502402302
- Page 63 and 64:
Table 19d: Jet-A 4658:DistillateVol
- Page 65 and 66:
Density Measurements of Compressed
- Page 67 and 68:
270.00 15.155 819.16 370.00 2.027 7
- Page 69 and 70:
310.00 1.009 792.38 430.00 10.023 7
- Page 71 and 72:
410.0 0.99 706.3 450.0 0.99 672.941
- Page 73 and 74:
Jet-A-3602860840820Density [kg/m3]8
- Page 75 and 76:
Jet-A-4658860840820Density [kg/m3]8
- Page 77 and 78:
S-8Density [kg/m3]80078076074072070
- Page 79 and 80:
Table 26: Viscosity Measurements fo
- Page 81 and 82:
-1 / mm2·s T3.53.02.52.01.51.00.50
- Page 83 and 84:
-1 / mm2·s T4.03.53.02.52.01.51.00
- Page 85 and 86:
Figure 38: Measurements of the kine
- Page 87 and 88:
0.1250.1200.115 / W . m -1 K -10.11
- Page 89 and 90:
Heat Capacities of Jet Fuels S-8 an
- Page 91 and 92:
Figure 44: Heat capacity at constan
- Page 93 and 94:
incorporated earlier work on the th
- Page 95 and 96:
Table 29. Composition of the Surrog
- Page 97 and 98:
100*(ρ calc -ρ exp )/ρ exp10.80.
- Page 99 and 100:
Temperature, K530520510500490480470
- Page 101 and 102:
Table 30. Composition of surrogate
- Page 103 and 104:
76Deviations in Viscosity for S-8 S
- Page 105 and 106:
15. Bruno, T. J.; Smith, B. L., Ent
- Page 107 and 108:
41. Lemmon, E. W., McLinden, M.O.,
- Page 109 and 110:
Table A1. Thermal conductivity of J
- Page 111 and 112:
4025 361.405 358.992 10.175 0.1060
- Page 113 and 114:
7069 423.137 420.483 40.306 0.1104
- Page 115 and 116:
11033 502.232 500.622 20.338 0.0966
- Page 117 and 118:
4031 358.276 359.984 20.197 0.1111
- Page 119 and 120:
8005 439.412 441.678 0.290 0.0921 0
- Page 121 and 122:
11049 498.979 501.252 30.444 0.1013
- Page 123 and 124:
3067 338.230 340.876 40.410 0.1197
- Page 125 and 126:
7041 419.062 420.509 30.369 0.1092
- Page 127 and 128:
11027 499.803 502.171 10.287 0.0922
- Page 129 and 130:
1079 300.796 303.199 0.782 0.1316 0
- Page 131 and 132:
3035 404.815 406.980 20.455 0.1006
- Page 133 and 134:
4039 452.049 454.662 50.744 0.0997
- Page 135 and 136:
5047 495.554 497.822 0.783 0.0941 0
- Page 137 and 138:
6062 547.453 548.761 20.455 0.1043
- Page 139 and 140:
2033 320.952 322.769 19.953 4.255 0
- Page 141 and 142:
4037 358.681 361.505 10.216 4.058 0
- Page 143 and 144:
6021 399.683 401.387 5.081 3.862 0.
- Page 145 and 146:
8047 440.149 442.511 30.295 3.883 0
- Page 147:
11035 501.409 503.383 15.116 3.540