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Computational study of supersonic flow past non-stationary obstructions. II: Moving protrusion - MaRDI portal

Computational study of supersonic flow past non-stationary obstructions. II: Moving protrusion (Q1683354)

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scientific article; zbMATH DE number 6816377
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Computational study of supersonic flow past non-stationary obstructions. II: Moving protrusion
scientific article; zbMATH DE number 6816377

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    Computational study of supersonic flow past non-stationary obstructions. II: Moving protrusion (English)
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    8 December 2017
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    Summary: For an upward moving protrusion, recirculation regions develop on both sides with separation/reattachment distances increasing with protrusion height while being smaller than the corresponding fixed protrusion values. Differences in upstream wall pressures between moving versus fixed protrusions are reasoned in terms of: 1) extent of coalescence of upstream travelling compression waves into a shock; 2) inclination of this shock wave with free stream; 3) a low velocity high pressure band of fluid formed adjacent to the protrusion fore surface. Downstream wall pressures are lower than the corresponding fixed protrusion values due to a higher expansion of the flow for the range of protrusion heights considered. For an oscillating protrusion, wall pressure response to varying protrusion heights displays a hysteretic behaviour. Compressive/expansive effects generated during the protrusion's upward/downward motions persist after the protrusion changes its direction. Higher upstream and lower downstream wall pressures are observed in general at higher protrusion velocities. For Part I, see [the authors, ibid. 15, No. 3, 144--156 (2015; Zbl 1375.76059)].
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    shock wave boundary layer interaction
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    SWBLI
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    pressure hysteresis
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    particle velocity upwinding scheme
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    PVUS
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