Accession Number : AD0865239
Title : User's Manual for Subsonic-Transonic Flow Analysis (DECK 4). Supplement 4.
Corporate Author : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT
Report Date : 31 JUL 1966
Pagination or Media Count : 46
Abstract : A numerical procedure developed to treat two-dimensional subsonic-transonic flow through variable area passages has been programmed for the IBM 7094 computer. This machine's computational program numerically integrates the system of equations for a thermally perfect gas providing two capabilities. The first, a design mode, will calculate the geometric configuration so that a given velocity distribution is obtained along the centerline. The second, a performance mode, will calculate the flow field associated with a given geometric configuration. This report describes the equations and numerical techniques employed, presents flow charts and specific instructions for input formats and operation of the machine program.
Descriptors : *COMPUTER PROGRAMS), (*NOZZLE GAS FLOW, (*TWO DIMENSIONAL FLOW, SUBSONIC FLOW), NUMERICAL METHODS AND PROCEDURES, FLOW FIELDS, CONVERGENT DIVERGENT NOZZLES, VELOCITY, GEOMETRIC FORMS, NOZZLE THROATS, SUPERSONIC NOZZLES, EQUATIONS, DIGITAL COMPUTERS, SUBROUTINES, TRANSONIC FLOW, FLOW CHARTING.
Subject Categories : Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE