In isentropic flow of a perfect gas
(a) the velocity always decreases in conduits of increasing area.
(b) the velocity is always critical at the throat of a nozzle.
(c) if the flow is subsonic flow through a convergent nozzle, the maximum velocity is always at the throat.
(d) if the flow is in a convergent-divergent nozzle, the maximum velocity is always at the throat.
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