Accession Number:

AD0662775

Title:

NUMERICAL ANALYSIS OF A METHOD FOR CALCULATING THREE-DIMENSIONAL SUPERSONIC FLOW FIELDS.

Descriptive Note:

Final technical rept.,

Corporate Author:

ALABAMA UNIV HUNTSVILLE RESEARCH INST

Personal Author(s):

Report Date:

1967-08-01

Pagination or Media Count:

102.0

Abstract:

The stability and error of a method of near-characteristics computer program are studied. A scheme for almost second-order integration of the equations and a rapidly convergent shock calculation method are proposed. In addition, a technique to insure automatic fulfillment of the CFL condition is described. Author

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE