Accession Number:

AD0263103

Title:

CALCULATION OF SUPERSONIC FLOW AROUND AXISYMMETRIC FLARES

Descriptive Note:

Corporate Author:

TRW SPACE TECHNOLOGY LABS LOS ANGELES CALIF

Personal Author(s):

Report Date:

1958-05-21

Pagination or Media Count:

1.0

Abstract:

A machine program for the computation of supersonic flow around an axisymmetric flare is described. The computation consists of the following parts 1 The oblique shock problem in which upstream flow properties vary with position. 2 Calculation of the initial shock angle at the compression corner. 3 Insertion of characteristics for uniformity of mesh size.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE