Elements of Propulsion: Gas Turbines and Rockets

| T | f = 0 | f = 0.0169 | f = 0.0338 | f = 0.0507 | f = 0.0676 | ||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| K | C | h, kJ/kg | P r | h, kJ/kg | P r | h, kJ/kg | P r | h, kJ/kg | P r | h, kJ/kg | P r |
| 170 | -103 | 169.80 | 0.1903 | 170.82 | 0.1870 | 171.81 | 0.1840 | 172.76 | 0.1810 | 173.69 | 0.1783 |
| 180 | -93 | 179.85 | 0.2324 | 180.95 | 0.2288 | 182.01 | 0.2254 | 183.04 | 0.2221 | 184.03 | 0.2190 |
| 190 | -83 | 189.90 | 0.2809 | 191.08 | 0.2769 | 192.22 | 0.2731 | 193.33 | 0.2695 | 194.40 | 0.2661 |
| 200 | -73 | 199.93 | 0.3361 | 201.21 | 0.3318 | 202.44 | 0.3278 | 203.63 | 0.3239 | 204.79 | 0.3202 |
| 210 | -63 | 209.96 | 0.3985 | 211.34 | 0.3941 | 212.66 | 0.3899 | 213.95 | 0.3859 | 215.19 | 0.3821 |
| 220 | -53 | 219.99 | 0.4688 | 221.47 | 0.4644 | 222.89 | 0.4602 | 224.28 | 0.4561 | 225.62 | 0.4522 |
| 230 | -43 | 230.01 | 0.5475 | 231.60 | 0.5433 | 233.13 | 0.5392 | 234.62 | 0.5352 | 236.06 | 0.5315 |
| 240 | -33 | 240.02 | 0.6352 | 241.73 | 0.6313 | 243.38 | 0.6276 | 244.98 | 0.6240 | 246.53 | 0.6205 |
| 250 | -23 | 250.04 | 0.7325 | 251.87 | 0.7292 | 253.64 | 0.7260 | 255.36 | 0.7230 | 257.02 | 0.7201 |
| 260 | -13 | 260.05 | 0.8399 | 262.01 | 0.8376 | 263.91 | 0.8353 | 265.75 | 0.8331 | 267.53 | 0.8310 |
| 270 | -3 | 270.07 | 0.9581 | 272.17 | 0.9571 | 274.19 | 0.9561 | 276.16 | 0.9551 | 278.06 | 0.9542 |
| 280 | 7 | 280.08 | 1.0878 | 282.32 | 1.0885 | 284.49 | 1.0891 | 286.58 | 1.0898 | 288.61 | 1.0904 |
| 290 | 17 | 290.10 | 1.2296 | 292.49 | 1.2325 | 294.79 | 1.2352 | 297.03 | 1.2379 | 299.19 | 1.2406 |
| 300 | 27 | 300.13 | 1.3841 | 302.66 | 1.3897 | 305.11 | 1.3952 | 307.49 | 1.4005 | 309.79 | 1.4056 |
| 310 | 37 | 310.15 | 1.5521 | 312.85 | 1.5611 | 315.45 | 1.5699 | 317.97 | 1.5783 | 320.41 | 1.5865 |
| 320 | 47 | 320.19 | 1.7344 | 323.04 | 1.7474 | 325.80 | 1.7601 | 328.47 | 1.7724 | 331.05 | 1.7844 |
| 330 | 57 | 330.23 | 1.9315 |