Table 6.

Cooling Reynolds and Mach numbers and the corresponding coolant total pressures and temperatures.

${\text{Re}}_{\mathit{dc}}(-)$	$M_c(\%)$	$\frac{p_{0cooling}}{p_{01}}(-)$	$\frac{T_{0cooling}}{T_{01}}(\%)$
$1.00\times {10}^4$	0.85	0.915	0.334
$1.00\times {10}^4$	0.70	0.802	0.272
$1.00\times {10}^4$	1.00	2.022	0.720
$0.50\times {10}^4$	0.85	0.940	0.645
$1.50\times {10}^4$	0.85	0.898	0.231
$0.50\times {10}^4$	0.70	0.813	0.519
$1.50\times {10}^4$	0.70	0.800	0.192
$0.50\times {10}^4$	1.00	2.560	1.750
$1.50\times {10}^4$	1.00	2.175	0.500