A study is presented of the oblique interaction of both a step shock in unreacted explosive and a resolved reaction zone detonation with a rigid wedge. Two condensed- phase detonation models are considered: 1) a polytropic EOS model (Aslam-Bdzil- Stewart (ABS)) and 2) a simple JWL EOS-based model (Ignition & Growth (IG)). For the non-reactive polytropic model, we find good agreement between shock-polar theory and direct numerical simulation (DNS) results, for all wedge angles. For the nonreactive Ignition & Growth model, shock-polar theory agrees with DNS results only for the case of larger wedge angles. For smaller wedge angles, a non-classical curved Mach reflection is observed, reminiscent of von Neumann Mach reflection [5], which does not agree with three-shock polar theory. For small to moderate wedge angles, our resolved reaction zone detonation simulations show very curved Mach stems (and no obvious slip line) for both models. The strong influence that the explosives’ heat-release rate has on streamline curvature, explains the difference between the nonreactive and resolved reaction zone model results.
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机译:用等离子体约束实现重力场的动态控制热核聚变(TLTS)方法,通过热辐射等离子体绝缘的壁反应堆防止中子辐射并节省磁场和等离子体的混合,使用旋转磁场的异步磁惯性约束反应堆(AMITYAR和HFM)为实施该方法,在该反应器中点燃热核反应的方法,爆炸式等离子发生器(VIP)的实施方法,以及具有HFM的特立普安瓿,以实现D + T反应和具有超高温热度的HFM D +3НЕ和1Н+11В的高温反应