Accession Number : AD0631401

Title :   FLOW IN A DELAVAL NOZZLE BY THE GARABEDIAN METHOD.

Descriptive Note : Scientific rept.,

Corporate Author : AEROSPACE RESEARCH LABS OFFICE OF AEROSPACE RESEARCH WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Armitage,John V.

Report Date : JAN 1966

Pagination or Media Count : 92

Abstract : The problem of computing the flow in a deLaval nozzle when an initial velocity is specified along the axis of symmetry is considered. Fortran II programs are presented for computing the flow pattern in the subsonic region, for extrapolating the data to the sonic line, for extrapolating from the sonic line into the supersonic region, and for extending the computation into the supersonic region. (Author)

Descriptors :   (*LAVAL NOZZLES, NOZZLE GAS FLOW), (*NOZZLE GAS FLOW, MATHEMATICAL ANALYSIS), PARTIAL, COMPUTER PROGRAMMING, MATHEMATICAL PREDICTION, SUBSONIC FLOW, TRANSONIC FLOW, SUPERSONIC FLOW, AXIALLY SYMMETRIC FLOW

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE