On the existence of self-similar solutions in the supercritical region on a delta wing in a hypersonic flow

zbMath0903.76049MaRDI QIDQ1385814

G. N. Dudin

Publication date: 11 January 1999

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

boundary layer parametersfreestream stagnation temperaturestrong viscous interaction regime

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Related Items (3)

Formation of supercritical flow regions on low-aspect-ratio wings ⋮ Gas injection from the surface of a triangular plate in a hypersonic flow ⋮ Influence of intense surface cooling on hypersonic viscous flow past a delta wing

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