Engineering, 11.07.2019 04:10 jandrew8007
Ideal ramjet engine with inlet conditions 98kpa, 255k with y=1.4 and mach numb velocity of the diffuser is taking to a negligible velocity. on the basis of an cold air determine the temperature and pressure at the diffuser exit. hint mach number is m=v/c and c is speed of sound and c=(yrt)^2
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Ideal ramjet engine with inlet conditions 98kpa, 255k with y=1.4 and mach numb velocity of the diffu...
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