please answer this. ...........
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Hey here is your answer
We know that ,
Pressure = Thrust/Area
= 30/120
0.25 Nm2 or Pascal
I HOPE IT WILL YOU☺️☺️
Thanx for asking ur question ✌️✌️
We know that ,
Pressure = Thrust/Area
= 30/120
0.25 Nm2 or Pascal
I HOPE IT WILL YOU☺️☺️
Thanx for asking ur question ✌️✌️
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