Publication Date:
2019-07-12
Description:
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.
Keywords:
MECHANICS
Type:
ARC-12146
,
NASA Tech Briefs (ISSN 0145-319X); 14; 5; P. 73
Format:
text
Permalink