A contribution to the computation of transonic supersonic flows over blunt bodies

DOI10.1016/0045-7930(81)90022-0zbMath0466.76056OpenAlexW2066975158MaRDI QIDQ1155472

S. H. Smith

Publication date: 1981

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(81)90022-0

zbMATH Keywords

densitystagnation pointstationaryinviscidblunt bodiesbow shocksconservation of the total enthalpylimiting characteristicslines of constant pressureMach numberssonic linesspheres, ellipsoids, and hemisphere- cylinderstime-dependent finite-difference procedure

Mathematics Subject Classification ID

Transonic flows (76H05) Supersonic flows (76J20) Numerical solution of discretized equations for boundary value problems involving PDEs (65N22)

Cites Work

• An implicit finite-difference algorithm for hyperbolic systems in conservation-law form
• Calculation of three-dimensional stationary supersonic flow fields by applying the progonka process to a conservative formulation of the governing equations
• Iterative solution of transonic flows over airfoils and wings, including flows at mach 1
• Time-Split Finite-Volume Method for Three-Dimensional Blunt-Body Flow
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