Accession Number : AD0857980
Title : Fortran Program to Obtain Aerodynamic Coefficients from Pressure Distributions Output by the GASL Three-Dimensional Method of Characteristics Program.
Descriptive Note : Technical rept.,
Corporate Author : ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AER OBALLISTICS DIRECTORATE
Personal Author(s) : Marks, Alma S.
Report Date : 02 JUL 1969
Pagination or Media Count : 44
Abstract : A FORTRAN IV computer program is described which determines the local and integrated aerodynamic coefficients from local pressure data taken directly from the output tapes generated by the General Applied Science Laboratory's three-dimensional method of characteristics program. Computational results for a spherically blunted or sharp-nosed body of revolution with or without flare, at angle of attack, may be used. The report includes equations, FORTRAN statements, and examples for using the program. (Author)
Descriptors : *COMPUTER PROGRAMS), (*REENTRY VEHICLES, MATHEMATICAL MODELS), (*AERODYNAMICS, BLUNT BODIES, PRESSURE, DISTRIBUTION, THREE DIMENSIONAL FLOW, ANGLE OF ATTACK, BODIES OF REVOLUTION, CONICAL BODIES, AERODYNAMIC CHARACTERISTICS, NOSE CONES.
Subject Categories : Computer Programming and Software
Guided Missile Reentry Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE