Computation of unsteady transonic flow over a fighter wing using a zonal Navier-Stokes/full-potential method

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1097-0363(19990315)29:5<575::AID-FLD801>3.0.CO;2-2" /><575::AID-FLD801>3.0.CO;2-2 10.1002/(SICI)1097-0363(19990315)29:5<575::AID-FLD801>3.0.CO;2-2zbMath0951.76055OpenAlexW2043814972MaRDI QIDQ4264592

Olympio Achilles, Faria Mello, Lakshmi N. Sankar

Publication date: 13 December 2000

Full work available at URL: https://doi.org/10.1002/(sici)1097-0363(19990315)29:5<575::aid-fld801>3.0.co;2-2

zbMATH Keywords

Navier-Stokes equationsfinite difference methodtransonic flowshybrid methodF-5 wingfull-potential equationalternating-direction implicit approximate factorisation procedureunsteady compressible viscous flowsviscous/inviscid interface boundary conditions

Mathematics Subject Classification ID

Transonic flows (76H05) Finite difference methods applied to problems in fluid mechanics (76M20) Viscous-inviscid interaction for compressible fluids and gas dynamics (76N17)

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