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Aircraft Propulsion, 2nd Edition
book

Aircraft Propulsion, 2nd Edition

by Saeed Farokhi
May 2014
Intermediate to advanced
1048 pages
34h 57m
English
Wiley
Content preview from Aircraft Propulsion, 2nd Edition

APPENDIX A U.S. Standard Atmosphere

U.S. Standard Atmosphere U.S. Units

In this table alt is altitude in thousands of feet.

sigma is density divided by sea-level density.

delta is pressure divided by sea-level pressure.

theta is temperature divided by sea-level temperature.

temp is temperature in degrees Rankine.

press is pressure in pounds per square foot.

dens is density in slugs per cubic foot.

a is the speed of sound in feet per second.

visc is viscosity in 10−6 slugs per foot-second.

k.visc is kinematic viscosity in 10−6 square feet per second.

ratio is speed of sound divided by kinematic viscosity times 106.

Sea-level density = 0.0023769 slugs per cubic foot

Sea-level temperature = 518.7 degree Rankine

Sea-level pressure = 2116.2 pounds per square foot

alt sigma delta theta temp press dens a visc k.visc ratio
−1 1.0296 1.0367 1.0069 522.2 2193.8 0.0024472 1120.3 0.376 1.54E–4 7.30
  0 1.0000 1.0000 1.0000 518.7 2116.2 0.0023769 1116.5 0.374 1.57E–4 7.10
  1 0.9711 0.9644 0.9931 515.1 2040.9 0.0023081 1112.6 0.372 1.61E–4 6.91
  2 0.9428 0.9298 0.9863 511.5 1967.7 0.0022409 1108.7 0.370 1.65E–4 6.72
  3 0.9151 0.8963 0.9794 508.0 1896.7 0.0021752 1104.9 0.368 1.69E–4 6.54
  4 0.8881 0.8637 0.9725 504.4 1827.7 0.0021109 1101.0 0.366 1.73E–4 6.36
  5 0.8617 0.8321 0.9656 500.8 1760.9 0.0020482 1097.1 0.364 1.78E–4 6.18
  6 0.8359 0.8014 0.9588 497.3 1696.0 0.0019869 1093.2 0.362 1.82E–4 6.01
  7 0.8107 0.7717 0.9519 493.7 1633.1 0.0019270 1089.3
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