Separated supersonic flow past a trailing edge at incidence

DOI10.1016/0045-7930(86)90003-4zbMath0592.76087OpenAlexW1982246627MaRDI QIDQ1075873

B. George

Publication date: 1986

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

Full work available at URL: https://doi.org/10.1016/0045-7930(86)90003-4

zbMATH Keywords

shooting techniqueflow reversalsabrupt reattachmentavoidance of a catastrophic stallcatastrophic stallone-sided regular separationstall-free separated flowstrong downwash in the near-wakeSupersonic laminar flowthin trailing edgetriple-deck viscous-inviscid interactionswindward differencing

Mathematics Subject Classification ID

Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

Related Items (2)

The interactive breakdown in supersonic ramp flow ⋮ Laminar hypersonic leading edge separation – a numerical study

Cites Work

• The interaction of a shock wave with a laminar boundary layer
• Interacting flow theory and trailing edge separation – no stall
• A structure for laminar flow past a bluff body at high Reynolds number
• New, quasi-simultaneous method to calculate interacting boundary layers
• Correlated unsteady and steady laminar trailing-edge flows
• D’Alembert’s Paradox
• On self‐induced separation II
• Numerical and asymptotic solutions for the supersonic flow near the trailing edge of a flat plate at incidence
• Self-induced separation
• On slot injection into a supersonic laminar boundary layer

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