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- W4253525478 abstract "A numerical method (inverse method) was developed for gas-particle supersonic flow past axisymmetric blunt bodies. This method is based on a stream function coordinate system, which makes it convenient for determining the shock layer flowfields and body shapes. In using the present method, the gas-solid particle flows in the shock layers around blunt bodies (nearly spheres) were solved for freestream Mach number M∞=2. The effects of freestream loading ratio and particle diameter on the shock layer thickness, the body surface pressure and the flow quantities along the stagnation streamline are shown, and the flow patterns (gas streamlines and particle streamlines) in the shock layers are also shown." @default.
- W4253525478 created "2022-05-12" @default.
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- W4253525478 date "1984-01-01" @default.
- W4253525478 modified "2023-09-30" @default.
- W4253525478 title "A Numerical Study of Gas-Particle Supersonic Flow Past Blunt Bodies : The Case of Axisymmetric Flow" @default.
- W4253525478 doi "https://doi.org/10.1299/kikaib.50.185" @default.
- W4253525478 hasPublicationYear "1984" @default.
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