Accession Number : AD0824053
Title : A MATHEMATICAL MODEL FOR DENSITY, PRESSURE, AND MACH NUMBER AS FUNCTIONS OF ALTITUDE.
Descriptive Note : Technical rept.,
Corporate Author : NAVAL AVIONICS FACILITY INDIANAPOLIS IN
Personal Author(s) : Neyman, Roy
Report Date : 01 NOV 1967
Pagination or Media Count : 47
Abstract : This report contains empirical formulae for the computation of atmospheric density, atmospheric pressure, and mach number as functions of altitude. These formulae were obtained by fitting curves to the data given in U.S. Standard Atmospheres. Tabulation of computed values of density, pressure, and mach number and the error between these computed values and the corresponding values listed in U.S. Standard Atmospheres are given for altitudes ranging from 0 to 70,000 feet. (Author)
Descriptors : (*METEOROLOGICAL PHENOMENA, MATHEMATICAL MODELS), MACH NUMBER, BAROMETRIC PRESSURE, DENSITY, TROPOSPHERE, ALTITUDE, FUNCTIONS(MATHEMATICS), SIMULATION, FLIGHT, EQUATIONS, DIFFERENTIAL EQUATIONS, LEAST SQUARES METHOD, COMPUTER PROGRAMS, DIGITAL COMPUTERS, ERRORS, STRATOSPHERE.
Subject Categories : Aerodynamics
Statistics and Probability
Distribution Statement : APPROVED FOR PUBLIC RELEASE