Accession Number : AD0865238
Title : User's Manual for General Supersonic Flow Analysis (DECK 1). Supplement 1.
Corporate Author : PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT
Report Date : 31 JUL 1966
Pagination or Media Count : 72
Abstract : A machine computational program designed to treat all aspects of internal nozzle flow has been developed for use on the I.B.M. 7094 Computer at the Air Force Systems Command, Wright-Patterson Air Force Base, Ohio. The program constructs flow fields for both single or dual supersonic flows with or without shocks. This report describes the equations and numerical techniques employed and presents flow charts and specific instructions for input formats and operation of the machine program. Also included is a discussion of the fitting procedure incorporated in the program and a description of a test case with sample input and output.
Descriptors : *COMPUTER PROGRAMS), (*NOZZLE GAS FLOW, (*SUPERSONIC NOZZLES, FLOW FIELDS), PRESSURE, SHOCK WAVES, FLOW SEPARATION, BASE FLOW, BOUNDARY LAYER, HEAT TRANSFER, SKIN FRICTION, DRAG, THICKNESS, BELL NOZZLES, EXHAUST NOZZLES, VISCOSITY, WALLS, EQUATIONS, FLOW CHARTING, INPUT OUTPUT DEVICES, SUBROUTINES, NUMERICAL METHODS AND PROCEDURES.
Subject Categories : Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE