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Nonlinear damping model for supersonic air-intake buzz

Suryanarayana, GK and Singh, DB and Surya, Sumukh and Jagadeesh, G (2022) Nonlinear damping model for supersonic air-intake buzz. In: Aerospace Science and Technology, 126 (107567). ISSN 12709638

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Official URL: https://doi.org/10.1016/j.ast.2022.107567

Abstract

Air-intake buzz was initiated at Mach number of 3.0 on a two-dimensional isolated air-intake model in a wind tunnel by throttling the exit area. Schlieren images of shock oscillation around the intake entry during buzz were recorded using a high-speed camera. The recordings show a strong coupling between the bow-shock at the cowl lip and the oblique shock from the ramp. Image analyses were carried out, considering each image as a matrix of pixels and the change of intensity of light analyzed. A dominant frequency of 103.8 Hz (Strouhal no = 0.008 based on throat height) associated with the shock oscillations and harmonics of the shock oscillations are indicated. Phase-plots of the intensity and the rate of change of intensity show nearly perfect ellipse after filtering at the dominant frequency. Thus, the buzz phenomenon is associated with a limit-cycle oscillation as in a nonlinear Van-Der Pol oscillator. The computed damping factor synchronizes with the amplitude at all times, establishing that buzz is a stable and self-sustained oscillation with equilibrium between inertial and damping forces. It is proposed that a control scheme based on feed-forward control system using a suitable forcing function could be mathematically developed to suppress supersonic air-intake buzz.

Item Type: Journal Article
Publication: Aerospace Science and Technology
Publisher: Elsevier Masson s.r.l.
Additional Information: The copyright of this article belongs to the Elsevier Masson s.r.l.
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Date Deposited: 24 May 2022 08:55
Last Modified: 24 May 2022 08:55
URI: https://eprints.iisc.ac.in/id/eprint/72329

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