Surface pressure fluctuation generated by a jet impinging on a curved plate

Ho, Chih‐Ming; Plocher, Dennis; Leve, Howard L.

doi:10.2514/6.1977-114

Cited by 2 publications

(1 citation statement)

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“…Their measurements suggest that a finite-length stagnation line, instead of a stagnation point, exists on the plate. The surface pressure fluctuations on curved plates impinged upon by an axisymmetric jet were measured by Ho, Plocher & Leve (1977). The general characteristics of the fluctuating pressure, such as the normalized maximum fluctuation level, the peak frequency and the roll-off exponent of the spectra, do not change with the geometry of the plate.…”

Section: Introductionmentioning

confidence: 99%

Dynamics of an impinging jet. Part 1. The feedback phenomenon

1981

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In a high-speed subsonic jet impinging on a flat plate, the surface pressure fluctuations have a broad spectrum due to the turbulent nature of the high-Reynolds-number jet. However, these pressure fluctuations dramatically change their pattern into almost periodic waves, if the plate is placed close to the nozzle (x0/d < 7·5). In the present study extensive measurements of the near-field pressure provide solid support for the hypothesis that a feedback mechanism is responsible for the sudden change observed in the pressure fluctuations at the onset of resonance. The feedback loop consists of two elements: the downstream-convected coherent structures and upstream-propagating pressure waves generated by the impingement of the coherent structures on the plate. The upstream-propagating waves and the coherent structures are phase-locked at the nozzle exit. The upstream-propagating waves excite the thin shear layer near the nozzle lip and produce periodic coherent structures. The period is determined by the convection speed of the coherent structures, the speed of the upstream-propagating waves as well as the distance between the nozzle and the plate. An instability process, herein referred to as the ‘collective interaction’, was found to be critical in closing the feedback loop near the nozzle lip.

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Section: Introductionmentioning

confidence: 99%