Theory of the hypersonic viscous shock layer at high Reynolds numbers and intensive injection of foreign gases

DOI10.1016/0021-8928(75)90091-XzbMath0319.76051OpenAlexW1645526292MaRDI QIDQ1223004

È. A. Gershbeĭn

Publication date: 1974

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(75)90091-x

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

Related Items

Investigation of a three-dimensional hypersonic viscous shock layer in the stagnation point neighborhood in the presence of injection or suction ⋮ A three-dimensional hypersonic viscous shock layer in two-phase flow ⋮ On the theory of a three-dimensional, viscous hypersonic shock layer in the neighbourhood of the plane of symmetry

Cites Work

• Asymptotic solution of the equations of a laminar multicomponent boundary layer with intensive suction
• The effect of a magnetic field on Stokes flow in a conducting fluid
• Errata: "Boundary-Layer Flows with Large Injection and Heat Transfer"
• Supersonic flow past a finite cone with large surface mass injection.
• On some properties of supersonic conical gas flow
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