Answer / seenu

1

Answer / vimal

=1

Answer / nilesh

at throat=1

Answer / k

at the nozzle throat, mass flow rate is maximum therefore
the throat is sonic and thus mach number is =1

Answer / chetan

it 'd be greater than one,
t reaches around approx. 1100 m/sec

Answer / karthick

equal to one

Answer / fisuleng09

NEARLY 1

Answer / karthick

the throat of the nozzle is always designed to have sonic
velocity i.e., mach number = 1

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