Analysis of three-dimensional inviscid supersonic flow between a body and an outer wall : with application to a jet stretcher system /

The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.Report was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.Final Report: July 1, 1973 -- June 30, 1975.""August 1976."Includes bibliographic references (page 15).The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.Mode of access: Internet