Publikationsdatum:
2019-06-28
Beschreibung:
This paper describes a method for doing direct simulation Monte Carlo (DSMC) calculations using parallel processing and presents some results of applying the method to several hypersonic, rarefied flow problems. The performance and efficiency of the parallel method are discussed. The applications described are the flow in a channel and the flow about a flat plate at incidence. The results show significant advantages of parallel processing over conventional scalar processing and demonstrate the scalability of the method to large problems.
Schlagwort(e):
AERODYNAMICS
Materialart:
AIAA PAPER 91-0772
Format:
text
