Accession Number : ADA313224

Title :   High Order Accuracy Computational Methods in Aerodynamics Using Parallel Architectures.

Descriptive Note : Final rept. 15 Jan 95-31 Mar 96,

Corporate Author : BROWN UNIV PROVIDENCE RI DIV OF APPLIED MATHEMATICS

Personal Author(s) : Gottlieb, David ; Shu, Chi-Wang ; Fischer, P. F. ; Don, W. S.

PDF Url : ADA313224

Report Date : 02 AUG 1996

Pagination or Media Count : 6

Abstract : The main theme of this research is the application of high order accurate schemes to complicated flow problems. The advantage of using high order schemes for long time simulations is widely recognized by now. Also for problems where fine details of the flow field have to be captured accurately the use of high accuracy schemes is mandatory. These two classes of problems encompass many of the current problems in scientific computing.

Descriptors :   *COMPUTATIONS, *ACCURACY, *PARALLEL PROCESSORS, *FLOW FIELDS, *AERODYNAMICS, COMPUTERIZED SIMULATION, HIGH RATE, SHOCK WAVES, COMPUTER ARCHITECTURE, PARALLEL PROCESSING, LONG RANGE(TIME).

Subject Categories : Numerical Mathematics
      Computer Hardware
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE