At the nozzle throat wats the value of mach no. >1 ,<1 ,=1

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At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / seenu

Is This Answer Correct ?

17 Yes

2 No

At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / vimal

Is This Answer Correct ?

14 Yes

3 No

At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / nilesh

at throat=1

Is This Answer Correct ?

3 Yes

0 No

At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / k

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

Is This Answer Correct ?

2 Yes

0 No

At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / chetan

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

Is This Answer Correct ?

3 Yes

2 No

At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / karthick

equal to one

Is This Answer Correct ?

1 Yes

0 No

At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / fisuleng09

NEARLY 1

Is This Answer Correct ?

1 Yes

1 No

At the nozzle throat wats the value of mach no. >1 ,<1 ,=1..

Answer / karthick

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

Is This Answer Correct ?

0 Yes

0 No

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