Physics, 30.09.2019 21:10 kyusra2008
Consider the purely subsonic flow in a convergent-divergent duct. the inlet, throat and exit area are l m^2, 0.7 m^2 and 0.85 m^2, respectively. if the inlet mach number and pressure are 0.3 and 0.8 times 10^5 n/m^2, respectively, calculate: a) m and p at the throat, (b) m and p at the exit.
Answers: 1
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Physics, 22.06.2019 18:30
Suppose you plot the distance traveled by an object at various times and you discover that the graph is not a straight line. what does this indicate about the object's acceleration?
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Consider the purely subsonic flow in a convergent-divergent duct. the inlet, throat and exit area ar...
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