Aircraft Engine Design, Second Edition

| Standard day | Cold day | Hot day | Tropic day | |||
|---|---|---|---|---|---|---|
| h | ? | ? | ? | ? | ? | h |
| (kft) | ( P/P std) | ( T/T std) | ( T/T std) | ( T/T std) | ( T/T std) | (kft) |
| 0 | 1.0000 | 1.0000 | 0.7708 | 1.0849 | 1.0594 | 0 |
| 1 | 0.9644 | 0.9931 | 0.7972 | 1.0774 | 1.0520 | 1 |
| 2 | 0.9298 | 0.9863 | 0.8237 | 1.0700 | 1.0446 | 2 |
| 3 | 0.8963 | 0.9794 | 0.8501 | 1.0626 | 1.0372 | 3 |
| 4 | 0.8637 | 0.9725 | 0.8575 | 1.0552 | 1.0298 | 4 |
| 5 | 0.8321 | 0.9656 | 0.8575 | 1.0478 | 1.0224 | 5 |
| 6 | 0.8014 | 0.9588 | 0.8575 | 1.0404 | 1.0150 | 6 |
| 7 | 0.7717 | 0.9519 | 0.8575 | 1.0330 | 1.0076 | 7 |
| 8 | 0.7429 | 0.9450 | 0.8575 | 1.0256 | 1.0002 | 8 |
| 9 | 0.7149 | 0.9381 | 0.8575 | 1.0182 | 0.9928 | 9 |
| 10 | 0.6878 | 0.9313 | 0.8565 | 1.0108 | 0.9854 | 10 |
| 11 | 0.6616 | 0.9244 | 0.8502 | 1.0034 | 0.9780 | 11 |
| 12 | 0.6362 | 0.9175 | 0.8438 | 0.9960 | 0.9706 | 12 |
| 13 | 0.6115 | 0.9107 | 0.8375 | 0.9886 | 0.9632 | 13 |
| 14 | 0.5877 | 0.9038 | 0.8312 | 0.9812 | 0.9558 | 14 |
| 15 | 0.5646 | 0.8969 | 0.8248 | 0.9738 | 0.9484 | 15 |
| 16 | 0.5422 | 0.8901 | 0.8185 | 0.9664 | 0.9410 | 16 |
| 17 | 0.5206 | 0.8832 | 0.8121 | 0.9590 | 0.9336 | 17 |
| 18 | 0.4997 | 0.8763 | 0.8058 | 0.9516 | 0.9262 | 18 |
| 19 | 0.4795 | 0.8695 | 0.7994 | 0.9442 | 0.9188 | 19 |
| 20 | 0.4599 | 0.8626 | 0.7931 | 0.9368 | 0.9114 | 20 |
| 21 | 0.4410 | 0.8558 | 0.7867 | 0.9294 | 0.9040 | 21 |
| 22 | 0.4227 | 0.8489 | 0.7804 | 0.9220 | 0.8965 | 22 |
| 23 | 0.4051 | 0.8420 | 0.7740 | 0.9145 | 0.8891 | 23 |
| 24 | 0.3880 | 0.8352 | 0.7677 | 0.9071 | 0.8817 | 24 |
| 25 | 0.3716 | 0.8283 | 0.7613 | 0.8997 | 0.8743 | 25 |
| 26 | 0.3557 | 0.8215 | 0.7550 | 0.8923 | 0.8669 | 26 |
| 27 | 0.3404 | 0.8146 | 0.7486 | 0.8849 | 0.8595 | 27 |
| 28 | 0.3256 | 0.8077 | 0.7423 | 0.8775 | 0.8521 | 28 |
| 29 | 0.3113 |