Numerical computations of supersonic inlet flow

DOI10.1002/fld.147zbMath1017.76062OpenAlexW2046540489MaRDI QIDQ2747797

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Publication date: 14 October 2001

Published in: International Journal for Numerical Methods in Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/fld.147

zbMATH Keywords

separationmass flow rateshock-boundary layer interactionshock reflectionsair-breathing propulsion systemshigh-speed space travelsupersonic inlet flow

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (1)

Viscous flow in a mixed compression intake

Cites Work

• A multi-surface method of coordinate generation
• Numerical Solutions of Supersonic and Hypersonic Laminar Compression Corner Flows
• Unnamed Item

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