Dala, Laurent, Combrinck, Madeleine, Lipatov, I.I. and Ustinov, I.N. (2021) The effect of the cone rotation in the supersonic gas flow on the velocity propagation of perturbations in the boundary layer. Acta Astronautica, 179. pp. 209-212. ISSN 0094-5765
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AA-D-20-00928_R1 (003).pdf - Accepted Version Available under License Creative Commons Attribution Non-commercial No Derivatives 4.0. Download (1MB) | Preview |
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.
Item Type: | Article |
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Uncontrolled Keywords: | Boundary layer, propagation of disturbances, supersonic, weak viscous-inviscid interaction, flow near a cone. |
Subjects: | F300 Physics H300 Mechanical Engineering H400 Aerospace Engineering |
Department: | Faculties > Engineering and Environment > Mechanical and Construction Engineering |
Depositing User: | Elena Carlaw |
Date Deposited: | 13 Oct 2020 08:10 |
Last Modified: | 12 Oct 2021 03:30 |
URI: | http://nrl.northumbria.ac.uk/id/eprint/44490 |
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