Numerical Study on Effects of Arrayed Pulsed Energy Depositions on a Supersonic Combustor

Table 3

Total pressure recovery coefficients.

Case	Case A	Case B	Case C	Case D	Case E	Case F	Case G	Case H	Case I
	0.8713	0.8659	0.8658	0.8643	0.8612	0.8637	0.8615	0.8645	0.8623