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)