For a nozzle
to convert subsonic flow into a supersonic flow, it must be -
Convergent
type
Divergent type
Convergent
divergent type
Of uniform
cross-sectional area
Convergent
divergent type
For a nozzle to convert subsonic flow into a supersonic flow, it must be
convergent divergent type. In a convergent divergent nozzle, the hot exhaust
leaves the combustion chamber and converges down to the minimum area, or
throat, of the nozzle.
Hence, the
correct option is (C).
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