Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control

In this appendix the properties of the 1962 U.S. Standard Atmosphere are tabulated in accordance with Eqs. (1.5 1.17) and (1.21 1.22) of Chapter 1. Two tables are given: Table B1 in English units and Table B2 in Metric units.
| Altitude | Temperature | Temperature ratio | Pressure | Pressure ratio | Density | Density ratio | Coefficient of viscosity | Speed of sound |
|---|---|---|---|---|---|---|---|---|
| h, ft | T, R | ? | P, psf | ? | | ? | | a, ft/s |
| 0 | 518.7 | 1.000 | 2116 | 1.000 | 2.377 | 1.000 | 3.737 | 1,116.4 |
| 1,000 | 515.1 | 0.9932 | 2041 | 0.9644 | 2.3081 | 0.97106 | 3.717 | 1,112.6 |
| 2,000 | 511.5 | 0.9863 | 1963 | 0.9298 | 2.2409 | 0.94277 | 3.697 | 1,108.7 |
| 3,000 | 508.0 | 0.9794 | 1879 | 0.8962 | 2.1751 | 0.91512 | 3.677 | 1,104.0 |
| 4,000 | 504.4 | 0.9725 | 1828 | 0.8637 | 2.1109 | 0.88809 | 3.657 | 1,101.0 |
| 5,000 | 500.8 | 0.9657 | 1761 | 0.8320 | 2.0481 | 0.86167 | 3.636 | 1,097.1 |
| 6,000 | 497.3 | 0.9588 | 1696 | 0.8014 | 1.9868 | 0.83586 | 3.616 | 1,093.2 |
| 7,000 | 493.7 | 0.9519 | 1633 | 0.7716 | 1.9268 | 0.81064 | 3.596 | 1,089.2 |
| 8,000 | 490.1 | 0.9459 | 1572 | 0.7428 | 1.8683 | 0.78602 | 3.575 | 1,085.3 |
| 9,000 | 486.6 | 0.9382 | 1513 | 0.7148 | 1.8111 | 0.76196 | 3.555 | 1,081.4 |
| 10,000 | 483.0 | 0.9313 | 1456 | 0.6877 | 1.7533 | 0.73848 | 3.534 | 1,077.4 |
| 11,000 | 479.4 | 0.9244 | 1400 | 0.6614 | 1.7008 | 0.71555 | 3.513 | 1,073.4 |
| 12,000 | 475.9 | 0.9175 | 1345 | 0.6360 | 1.6476 | 0.69317 | 3.493 | 1,069.4 |
| 13,000 | 472.3 | 0.9107 | 1293 | 0.6113 | 1.5957 | 0.67133 | 3.472 | 1,065.4 |
| 14,000 | 468.7 | 0.9038 | 1243 | 0.5857 | 1.5451 | 0.65003 | 3.451 | 1,061.4 |
| 15,000 | 465.2 | 0.8969 | 1194 | 0.5643 | 1.4956 | 0.62924 | 3.430 | 1,057.3 |
| 16,000 | 461.6 | 0.8900 | 1147 | 0.5420 | 1.4474 | 0.60896 | 3.409 | 1,053.2 |
| 17,000 | 458.0 | 0.8831 | 1101 | 0.5203 | 1.4004 | 0.58919 | 3.388 | 1,049.2 |
| 18,000 | 454.5 | 0.8763 | 1057 | 0.4994 | 1.3546 | 0.56991 | 3.366 | 1,045.1 |
| 19,000 | 450.9 | 0.8694 | 1014 |