Atmosphere Lecture 2 ME EN 415 Andrew Ning aning@byu.edu UCAR - - PowerPoint PPT Presentation
Atmosphere Lecture 2 ME EN 415 Andrew Ning aning@byu.edu UCAR - - PowerPoint PPT Presentation
Atmosphere Lecture 2 ME EN 415 Andrew Ning aning@byu.edu UCAR Altitude Geometric Altitude: Absolute Altitude: Pressure Altitude: Geopotential Altitude: Altimeters International Standard Atmosphere Geopotential Temperature Altitude
UCAR
Altitude
Geometric Altitude: Absolute Altitude: Geopotential Altitude: Pressure Altitude:
Altimeters
International Standard Atmosphere
Geopotential Altitude (km) Temperature Gradient (K/km)
- 6.5
11 0.0 20 +1.0 32 +2.8 47 0.0 51
- 2.8
71
- 2.0
84.8520
Temperature Altitude
Sea Level Properties TSL 288.15 K PSL 1.01325 × 105 Pa µSL 1.79 × 10−5 kg/m-s g 9.80665 m/s2
Hydrostatics
Isothermal Layers
Gradient Layers
Curve Fit
modified slightly from: Mark Drela, Flight Vehicle Aerodynamics
P(h) = PSL exp ✓ −0.118h − 0.0015h2 1 − 0.018h + 0.0011h2 ◆ applicable for altitudes below 47 km T(h) = TSL − 71.5 + 2.0 ln ⇥ 1 + exp(35.75 − 3.25h) + exp(−3.0 + 0.0003h3) ⇤ (h in km, T in K)
Upper Atmosphere NRLMSISE-00
(up to 1000 km)
Upper Atmosphere NRLMSISE-00
- r for a simple approximation during atmospheric entry:
(reasonable up to 140 km)
P PSL = exp−
gh RTm
(up to 1000 km)
Create Your Own
P, T, ρ = atmosphere(h)
More Comprehensive Databases
https://earth.nullschool.net ERA Interim dataset