- Consider A Normal Shock Wave In Air The Flow Upstream Of The Shock Cor Responds To A Standard Altitude Of 200 000 Ft A 1 (27.66 KiB) Viewed 11 times
Consider a normal shock wave in air. The flow upstream of the shock cor- responds to a standard altitude of 200,000 ft a
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Consider a normal shock wave in air. The flow upstream of the shock cor- responds to a standard altitude of 200,000 ft a
Consider a normal shock wave in air. The flow upstream of the shock cor- responds to a standard altitude of 200,000 ft at a Mach number of 25. Calculate the chemical species distributions in the nonequilibrium region behind the shock, as a function of distance behind the shock front. Plot your results graphically. Assume that the chemical species present are N₂, O₂, N, and O. (We will ignore NO and any ionization.)