|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: SCPro/ProEnvirons
% Computes the atmospheric density using scale heights above 80 km. Type AtmScaleHeightsStdAtm for a demo. Since version 8. -------------------------------------------------------------------------- Form: [rho, a, nu, p, t] = AtmScaleHeightsStdAtm( h, atmData ) -------------------------------------------------------------------------- ------ Inputs ------ h (1,:) Altitude (km) atmData (.) Atmosphere data, see AtmData.txt ------- Outputs ------- rho (1,:) Density (kg/m^3) a (1,:) Speed of sound (m/s) nu (1,:) Kinematic viscosity (N-s/m^2) p (1,:) Pressure (N/m^2) t (1,:) Temperature --------------------------------------------------------------------------
AerospaceUtils: AeroData/AtmData AerospaceUtils: AtmosphericCalculations/AtmDens2 Common: Atmosphere/StdAtm Common: Graphics/Plot2D
Back to the SCPro Module page