Complete 1976 Standard Atmosphere Matlab script

Publisher review:
Complete 1976 Standard Atmosphere calculates Temperature, Pressure, Density, Speed of Sound, Gravity, Dynamic/Kinematic Viscosity, k This is a complete model of the 1976 US standard atmosphere model with valid data between sea level and 1000 km. This set of functions returns Temperature, Pressure, Density, Speed of Sound, Gravity, Dynamic and Kinematic Viscosity, Coefficient of Thermal Conductivity, Gas Number Density at desired altitudes. Ability to convert to English Units as desired. Values DO differ by less than 1% due to different integration technique and should be closer to the actual values of the integrals described in the 1976 U.S. Standard Atmosphereatmo.m-main programatmo_compo.m-Gas composition for upper atmosphere programatmo_p.m-Pressure Computation Programatmo_temp.m-Temperature Computation Prgramf_n.m-Gas Composition Integral Programint_tau.m-Tau integral for Hydrogentester.m-Runs atmo.m code for complete atmosphere and does plots for each of the variables
Operating system:
Windows / Linux / Mac OS / BSD / Solaris

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