Sasidharan, V and Duvvuri, S (2021) Large- And small-amplitude shock-wave oscillations over axisymmetric bodies in high-speed flow. In: Journal of Fluid Mechanics .
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Abstract
The phenomena of self-sustained shock-wave oscillations over conical bodies with a blunt axisymmetric base subject to uniform high-speed flow are investigated in a hypersonic wind tunnel at Mach number. The flow and shock-wave dynamics is dictated by two non-dimensional geometric parameters presented by the three length scales of the body, two of which are associated with the conical forebody and one with the base. Time-resolved schlieren imagery from these experiments reveals the presence of two disparate states of shock-wave oscillations in the flow, and allows for the mapping of unsteadiness boundaries in the two-parameter space. Physical mechanisms are proposed to explain the oscillations and the transitions of the shock-wave system from steady to oscillatory states. In comparison with the canonical single-parameter problem of shock-wave oscillations over spiked-blunt bodies reported in literature, the two-parameter nature of the present problem introduces distinct elements to the flow dynamics. © The Author(s), 2021. Published by Cambridge University Press.
Item Type: | Journal Article |
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Publication: | Journal of Fluid Mechanics |
Publisher: | Cambridge University Press |
Additional Information: | The copyright for this article belongs to Cambridge University Press |
Keywords: | Wind tunnels, Axisymmetric bodies; Distinct elements; High speed flows; Hypersonic wind tunnels; Oscillatory state; Physical mechanism; Shock wave oscillation; Shock-wave dynamics, Shock waves |
Department/Centre: | Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering) |
Date Deposited: | 24 Mar 2021 09:22 |
Last Modified: | 24 Mar 2021 09:22 |
URI: | http://eprints.iisc.ac.in/id/eprint/68530 |
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