关于飞机爆炸的演变

J. F. Clarke, D. Kassoy, N. E. Meharzi, N. Riley, R. Vasantha
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引用次数: 40

摘要

本文利用可压缩可燃气体混合物平面一维非定常运动的Navier-Stokes方程的数值解,跟踪了由气体占据的有效半无限区域边界的固体表面上的大热量所引发的事件的历史。平面泽尔多维奇-冯·诺伊曼-多林爆炸最终要么出现在前驱激波(存在于每一组情况下),要么出现在前驱激波后面由不稳定感应域和最初准稳定快焰占据的区域。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
On the evolution of plane detonations
Numerical solutions of the Navier–Stokes equations for the plane one-dimensional unsteady motion of a compressible, combustible gas mixture are used to follow the history of events that are initiated by addition of large heat power through a solid surface bounding an effectively semi-infinite domain occupied by the gas. Plane Zel’dovich–von Neumann–Doring detonations eventually appear either at the precursor shock (which exists in every set of circumstances) or in the regions, occupied by an unsteady induction-domain and an initially quasi-steady fast-flame, that lie behind the precursor shock.
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