Review Article
Review on Recent Advances in Pulse Detonation Engines
Figure 17
Contour of axial flame temperature distribution generated by an accelerating flame in obstacle landed detonation tube for (a) BR = 0.4, (b) BR = 0.5, (c) BR = 0.6, and (d) BR = 0.7 at Ma = 5 for spacing of cm [132].
(a) |
(b) |
(c) |
(d) |