Two-phase mass injection from the stagnation zone of a blunt body in a hypersonic flow

DOI10.1007/BF01051325zbMath0789.76090OpenAlexW2073231778MaRDI QIDQ1317741

A. N. Osiptsov, E. G. Shapiro

Publication date: 12 April 1994

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

Full work available at URL: https://doi.org/10.1007/bf01051325

zbMATH Keywords

boundary layeraxisymmetric bodythin viscous shock layersimilarity parameterstwo-continuum model of a dusty gas

Mathematics Subject Classification ID

Multiphase and multicomponent flows (76T99) Hypersonic flows (76K05)

Related Items (3)

Flow properties of a dusty-gas point source in a supersonic free stream ⋮ Flows near stagnation points in non-orthogonally colliding disperse viscous flows ⋮ Hypersonic flow past a supersonic two-phase source

Cites Work

• Investigation of regions of unbounded growth of the particle concentration in disperse flows
• Boundary layer and heat transfer in a two-phase gas-evaporating droplet medium
• Numerical solution of the hypersonic viscous shock-layer equations
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