1989
DOI: 10.1007/bf01075169
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Unsteady supersonic flow past a sphere moving through a thermal inhomogeneity

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1993
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“…In the interaction between the reflected compression wave and the contact boundary the hot-gas region is intensively compressed both for a spherical temperature inhomogeneity and for a plane layer of hot gas (the velocity has a maximum at ~ -0.5). A similar observation was made in [6]. The interaction may be accompanied by the initiation of a short-lived reversed flow region.…”
Section: Shock Layer Dynamics For Unsteady Interaction With a Finite supporting
confidence: 66%
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“…In the interaction between the reflected compression wave and the contact boundary the hot-gas region is intensively compressed both for a spherical temperature inhomogeneity and for a plane layer of hot gas (the velocity has a maximum at ~ -0.5). A similar observation was made in [6]. The interaction may be accompanied by the initiation of a short-lived reversed flow region.…”
Section: Shock Layer Dynamics For Unsteady Interaction With a Finite supporting
confidence: 66%
“…Curve 4 was calculated with twice the usual number of grid points in both directions. The axisymmetric flow upstream of a sphere moving through a plane region of gas with normal density distribution was studied in [6]. To make a correct comparison, it was necessary to repeat the calculations made in [6] for a uniform density distribution.…”
Section: Shock Layer Dynamics For Unsteady Interaction With a Finite mentioning
confidence: 99%