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- W2023822418 abstract "The two-dimensional stationary flow configuration of four plane shock waves intersecting at a point has been calculated for a perfect gas of specific-heat ratio γ = 1.4. The configuration represents the mutual reflection of an initial pair of shock waves of arbitrary strengths. The ratio of the stronger initial shock strength to the weaker ranged from 1 to 100 in terms of the pressure ratios across the shock waves, with the strength of the weaker wave ranging from 1.1 to 10. Calculations were made at 10° intervals over the entire range of angles of incidence for which the four-shock configuration was possible. The ordinary weak solution was entirely machine calculated along with its extreme angle. The sonic angles were calculated by graphical interpolation from calculated flow Mach numbers. The sonic and extreme angles were found not to differ by more than 1.1° in the range of shock strengths used. A new family of solutions which exists for unequal shock strengths was discovered graphically by plotting the machine-calculated shock polars." @default.
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- W2023822418 date "1962-05-01" @default.
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- W2023822418 title "Four-Shock Configuration" @default.
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- W2023822418 doi "https://doi.org/10.1063/1.1706662" @default.
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