Exit velocity of ideal ramjet Post author:samrathmittal Post published:December 20, 2020 Post category:Aerospace Calculator / Propulsion Calculator For an ideal ramjet engine, the ratios of stagnation to static pressure at the exit and at the inlet are the same, with the consequence that the inlet and exit Mach numbers are also the same. You Might Also Like Minimum Lift Cofficient Calculator October 17, 2020 Stagnation Pressure using Mach Number Calculator October 19, 2020 True Air Speed Calculator by Mohit Kudal February 20, 2021