User's Manual for General Supersonic Flow Analysis (DECK 1). Supplement 1.
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 31, 1966
- Accession Number
- AD0865238
Entities
Organizations
- Pratt & Whitney