Comparative Assessment of Modified - Models for Scramjet Intake Flow Analysis

Table 6

Flow conditions according to altitudes and Mach numbers.

Altitude (km)	(Pa)	(K)		Unit Re (1/m)		Unit Re (1/m)
20	5529.85	216.69
			22.5	3734.67	216.69
25	2522.27	216.69
			27.5	1682.92	224.19
30	1158.33	231.61