Publikationsdatum:
2019-07-12
Beschreibung:
Supersonic flow about cone calculated accurately. Report presents theoretical basis of computer code solving parabolized Navier-Stokes equations of supersonic and hypersonic flow. For increased accuracy in resolution of details of strong aerodynamic shocks, code incorporates implicit, finite-volume, upwind numerical-integration scheme. Performs well in numerical simulations of flows around simple bodies.
Schlagwort(e):
MECHANICS
Materialart:
ARC-12146
,
NASA Tech Briefs (ISSN 0145-319X); 14; 5; P. 73
Format:
text
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