Calculation of the base pressure and enthalpy downstream of a plane or axisymmetric step in supersonic flow with allowance for the effect of the initial boundary layer

zbMath0953.76536MaRDI QIDQ1580111

R. K. Tagirov, M. K. Aukin

Publication date: 18 January 2001

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

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

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