Gas injection from the surface of a triangular plate in a hypersonic flow

DOI10.1007/BF02698794zbMath0960.76041MaRDI QIDQ1580155

G. N. Dudin

Publication date: 13 September 2000

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

zbMATH Keywords

laminar boundary layerhypersonic flowgas injectiontriangular platestrong viscous-inviscid interactionsubcritical flow regionssupercritical flow regions

Mathematics Subject Classification ID

Viscous-inviscid interaction for compressible fluids and gas dynamics (76N17) Hypersonic flows (76K05)

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Investigation of the effect of injection from a yawed plate with the spanwise-varied base pressure on the disturbance propagation in the regime of strong interaction

Cites Work

• Unnamed Item
• A method of calculating a regime of strong viscous interaction on a delta wing
• Influence of intense surface cooling on hypersonic viscous flow past a delta wing
• On the existence of self-similar solutions in the supercritical region on a delta wing in a hypersonic flow