On the Critical Behaviour of Exothermic Explosions in Class A Geometries

Table 6

Variation of 𝛿_cr and 𝜃_cr with respect to 𝜀 (cylinder).

𝑚	𝜀	𝛿cr	𝜃cr
−2	0.01	2.06415	1.58738
	0.1	3.01620	2.65419
0	0.01	2.02216	1.45337
	0.1	2.26129	1.80247
0.5	0.01	2.01192	1.41353
	0.1	2.13219	1.677327