Accession Number:

AD0752898

Title:

Axisymmetric Transonic Flow Calculations.

Descriptive Note:

Summary technical rept.,

Corporate Author:

ULTRASYSTEMS INC IRVINE CALIF

Personal Author(s):

Report Date:

1972-10-01

Pagination or Media Count:

69.0

Abstract:

L REPT.,SMasson,Bruce S. Friedman,Eugene DAAA21-72-C-0334PATR-4271projectiles, transonic characteristics, computer programs, wind tunnel models, flow fields, numerical methods and procedures, aerodynamic configurations, shock wavesaxisymmetric bodies, inviscid flowA computer program SONIC 2, was developed to calculate transonic flow about axisymmetric bodies. The code computes the exact, inviscid compressible flow field with or without shock waves, and it uses a body oriented mesh to permit the exact treatment of an arbitrary body shape. The numerical integration employs the method of Godunov to obtain a stable finite difference approximation to the flow equations. Several examples of results of the code are included along with comparisons to wind tunnel data. Author

Subject Categories:

  • Ammunition and Explosives
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE