Numerical study of the circular cylinder in supersonic ground effect conditions

Sugar-Gabor, O ORCID: 2018, 'Numerical study of the circular cylinder in supersonic ground effect conditions' , International Review of Aerospace Engineering, 11 (1) .

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A numerical study of the aerodynamics of a circular cylinder section in proximity to the ground surface was performed, for Mach numbers of 1.5 and 2.9 and ground clearances between 2 and 0.125, non-dimensional with respect to the cylinder diameter. The supersonic flow was computed using a finite-volume Reynolds-averaged Navier-Stokes solver, using adequately stabilized numerical schemes. The flow field computed in ground effect conditions was complex, and significantly varied as a function of both variables. The shape and standoff distance of the detached bow shock were very sensitive to changes in ground clearance. The velocity profile in the gap between the cylinder and ground showed significant interactions between the two boundary layers, and a gradually reduced supersonic expansion close the body surface.

Item Type: Article
Schools: Schools > School of Computing, Science and Engineering > Salford Innovation Research Centre
Journal or Publication Title: International Review of Aerospace Engineering
Publisher: Praise Worthy Prize
ISSN: 1973-7459
Related URLs:
Depositing User: O Sugar-Gabor
Date Deposited: 12 Feb 2018 15:30
Last Modified: 16 Feb 2022 18:37

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