Accession Number : AD0662775
Title : NUMERICAL ANALYSIS OF A METHOD FOR CALCULATING THREE-DIMENSIONAL SUPERSONIC FLOW FIELDS.
Descriptive Note : Final technical rept.,
Corporate Author : ALABAMA UNIV HUNTSVILLE RESEARCH INST
Personal Author(s) : Brainerd,Jerome J.
Report Date : AUG 1967
Pagination or Media Count : 102
Abstract : The stability and error of a method of near-characteristics computer program are studied. A scheme for 'almost' second-order integration of the equations and a rapidly convergent shock calculation method are proposed. In addition, a technique to insure automatic fulfillment of the CFL condition is described. (Author)
Descriptors : (*SUPERSONIC FLOW, *FLOW FIELDS), (*THREE DIMENSIONAL FLOW, NUMERICAL ANALYSIS), STABILITY, COMPUTER PROGRAMS, ERRORS, SHOCK WAVES
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE