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Numerical simulations were performed with a parallel computer to solve for the behaviour of the three-dimensional gas-solid two-phase detonation. The numerical method is a second-order modified Harten-Yee TVD upwind scheme and time integration uses a first order Euler integration. A two-step chemical reaction model represents the reaction of constarch-particles and oxygen. The numerical results show that a periodic two-headed detonation appears with a three-dimensional propagation mechaism before and after a triple point collisions. A comparison between the numerical and experimental results reveals that detonation velocity of numerical results agrees well with that of experimental results.
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Tom
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101--116
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Bibliogr. 26 poz., rys.
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- Tsuboi, N. - Research Division for Space Transportation, ISAS, Kanagawa, Japan Hayashi, A. K. - Dept. of Mech. Eng., Aoyama Gakuin Univ. Setagaya, Tokyo, Japan Matsumoto, Y. - Dept. of Mech. Eng., The University of Tokyo, Japan
Bibliografia
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Bibliografia
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bwmeta1.element.baztech-article-BWM2-0009-0029