Standard Atmosphere Computations This form calculates properties related to the 1976 standard atmosphere up to 230,000 ft. The code used is based on the original Javascript of Ilan Kroo (kroo@leland.stanford.edu) 31 Dec 95. Inputs Altitude Speed Reference Length   Tabulated Data and Downloads Results Temperature Density Pressure Speed of Sound Viscosity Mach Number Dynamic Pressure Critical Cp Vacuum Cp Reynolds Number Laminar Cf Turbulent Cf

Back to Properties of Atmosphere Section