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Titlebook: 31st International Symposium on Shock Waves 2; Applications Akihiro Sasoh,Toshiyuki Aoki,Masahide Katayama Conference proceedings 2019 Spri

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Methodology of the National ES Assessmental energy released to the kinetic energy of the material and energy dissipation during compaction of the porous particle bed. In the present paper, the effect of various parameters on the blast wave attenuation and profile during explosive particle dispersal is explored with a multiphase hydrocode.
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Religious Liberty or Religious Test?,a rapid transition to the detonation. In this study, numerical simulations are performed to investigate the dynamics of the deflagration-to-detonation transition (DDT) in the pulse detonation engines using aluminium particles. The DDT process and detonation wave propagation towards the unburnt hydro
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https://doi.org/10.1007/978-1-4039-8130-1sional (2D) compressible reactive Euler equations with a one-step chemical reaction model are solved by a well-validated upwind CE/SE scheme using up to 1.6 billion mesh points. Numerical results imply that one-dimensional (1D) approaches can only interpret the direct initiation mechanism of stable
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Religious Liberty or Religious Test?,on-to-detonation transition process (DDT), and detonation propagation process. These three processes often include a number of complex subprocesses, which strongly influence the performance characteristics of the engine. Thus, it is important to understand the physical and chemical insights of these
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A Celebration of Mathematical Modelingnum particles are spherical with a diameter range of 1–50 μm, using a particle concentration of 300 g/m. approximately. It is found that the single-front and double-front detonation waves can propagate in a mixture of . = 1.0 H.–air and aluminum particles which react with water vapor produced by gas
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Anthony C. Atkinson,Stephen E. Fienberg detonation completes in quite a short time. Therefore, many researches on detonation engines have been conducted around the world. An RDE can be used as a kick rocket motor for deep-space exploration. However, there are some problems to be solved prior to the practical use of an RDE. One of the mos
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