Accession Number:

AD0787272

Title:

Compressible Flow Solutions in Two Space Variables Using a Successive Perturbation Method.

Descriptive Note:

Technical rept.,

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL ALA AEROBALLISTICS DIRECTORATE

Personal Author(s):

Report Date:

1974-07-22

Pagination or Media Count:

26.0

Abstract:

The present work is the result of a study of the Spalding-Patankar pressure linked algorithm treated as a perturbation technique. The ease of use and demonstrated convergence of the method indicate that its extension or generalization might be fruitful in producing new relaxation procedures. This report describes the application of a relaxation method modeled on the pressure linked algorithm to two dimensional compressible flow.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE