The effect of the cone rotation in the supersonic gas flow on the velocity propagation of perturbations in the boundary layer

Laurent Dala, Madeleine Combrink, Igor Lipatov, I.N. Ustinov

Research output: Contribution to journalArticlepeer-review

Abstract

The paper aimed at studying the peculiarities of boundary layer on a rotating body. Rotation of axisymmetric bodies is often used for their stabilization at a high velocity motion in the atmosphere. Presented are calculation of boundary layer flow on a rotating cone at zero angle of attack. Longitudinal and full enthalpy profiles in the laminar boundary layer obtained as a result of calculations were used to determine upstream disturbances propagation velocity. New integral relation was determined to find out disturbances propagation velocity for the regime of weak hypersonic viscous-inviscid interaction. Effects of surface rotation velocity along with the temperature factor influence were investigated.
Original languageEnglish
Pages (from-to)209-212
Number of pages4
JournalActa Astronautica
Volume179
Early online date12 Oct 2020
DOIs
Publication statusPublished - 1 Feb 2021

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