what will be the change in pressure if the thrust and are will be increased double ?????
As you know,
Pressure (P)=(Thrust or Force)F/ Area(A)
If thrust and area both are doubled,
Then P'=2F / 2A=F/A=P
i.e Pressure remains same.
what will be the change in pressure if the thrust and are will be increased double ?????
As you know,
Pressure (P)=(Thrust or Force)F/ Area(A)
If thrust and area both are doubled,
Then P'=2F / 2A=F/A=P
i.e Pressure remains same.