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  • 1
    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
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  • 2
    Publication Date: 2019-07-12
    Description: Report discusses computational fluid dynamics (CFD) to simulate generation and propagation of sonic booms in near- and mid-field regions of supersonic flows about simplified bodies representative of advanced airplanes. Parabolized Navier-Stokes equations integrated by implicit, approximate-factorization, finite-volume algorithm in which crossflow inviscid fluxes evaluated by Roe's flux-difference-splitting scheme. Near-field solutions obtained by applying algorithm to flows immediately surrounding bodies. Solutions transferred to computer codes based on Whitham"s F-function theory for extrapolation to far-field.
    Keywords: MECHANICS
    Type: ARC-12855 , NASA Tech Briefs (ISSN 0145-319X); 16; 8; P. 58
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