1 / 8

1976 U.S. Standard Atmosphere

1976 U.S. Standard Atmosphere. One of several models of the atmosphere. Provides dependence of temperature, pressure and density on altitude. Temperature is tabulated at 8 specific altitudes and temperatures at other altitudes, pressure and density computed from those data. . P 1.

Jimmy
Download Presentation

1976 U.S. Standard Atmosphere

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. 1976 U.S. Standard Atmosphere • One of several models of the atmosphere. • Provides dependence of temperature, pressure and density on altitude. • Temperature is tabulated at 8 specific altitudes and temperatures at other altitudes, pressure and density computed from those data. 1976 US Standard Atmosphere

  2. P1 For Incompressible Fluid (like Water) P [Pascal = N/m2] The difference in pressure at the two depth is due to the weight of the column of water between them. Known as “hydrostatic equation” z 1976 US Standard Atmosphere

  3. Atmosphere – Compressible Fluid First consider an isothermal (constant temperature) atmosphere and assume a perfect gas: (Perfect gas) Rearrange: Apply limits: 1976 US Standard Atmosphere

  4. Atmosphere – Compressible Fluid So for isothermal (constant temperature) atmosphere: Note exponential drop of pressure with altitude, vs. linear with depth in an incompressible fluid like water. i.e., express pressure at one point in terms of that at a different altitude You can also handle (integrate) the case where the temperature is a linear function of altitude (constant “lapse rate”).* These are the two options in the VBA coding that goes with the USStandAtmos.xls spreadsheet on webpage (www.people.virginia.edu/~rjr/modules/xls) *See, e.g., D.G. Shepherd, Elements of Fluid Mechanics, Harcourt, Brace and World, 1965.

  5. Red circles indicate the limits of the 7 layers. Intermediate values are computed from them. 1976 US Standard Atmosphere

  6. U.S. Standard Atmosphere 1976 • Seven layers between sea level and ~85 km • Decrease of “g” with altitude is included in the calculation by use of “geopotential” altitude. • h = Altitude * Rearth / (Altitude + Rearth) • Two layers are isothermal • Five layers have constant “lapse rate” (dT/dz) • Pressure tabulated at base of each layer and change computed between there and the point of interest. • Use equation we just derived for isothermal layer, similar equation for constant lapse rate layers. • Density found from P and T and perfect gas law. 1976 US Standard Atmosphere

  7. Dependence of Density and Pressure On Altitude. • Handy numbers to remember: • Density of air at sea level [kg/m3], • Pressure at sea level [kPa], • Depth of troposphere [km]. 1976 US Standard Atmosphere

  8. Other notes: • Most sunlight comes through atmosphere (it’s largely transparent), hits surface of earth and the air in contact is heated up. That’s why the peak air temperature is at surface. • The other temperature peak at ~50 km is due to absorption of UV rays by ozone (and there isn’t much atmosphere there to heat up). 1976 US Standard Atmosphere

More Related