Force on a plate due to air jet

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    Air Force Jet Plate
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Suppose there is a plate with area A, on which jet of air with velocity 'v' is striking, then force on it will be = (density) * A* v^2

But if we go by basics i.e. F = d(mv)/dt = v d(m)/dt + m d(v)/ dt

here i am not able to figure out that why the second term i.e. m d(v)/ dt is zero, because when it becomes zero then only we will get the formula that i have written in second line.

Plz help.
 
You are also assuming that the jet is the same size as the plate (or larger than the plate). If it was smaller than the plate, then the A term would represent the area of the jet.

Anyway, look it a different way: as a conservation of linear momentum in a control volume. Initially, the rate of change of the momentum in the jet coming into this control volume is

[tex]\frac{d(\rho v)}{dt} = \rho \frac{dv}{dt} + v \frac{d \rho}{dt} = v \frac{d \rho}{dt} = \frac{F_{\textrm{plate}}}{V}[/tex]

Where [itex]\frac{dv}{dt}=0[/itex] because of the fact that [itex]v[/itex] coming into the control volume is not changing (the jet is coming at the plate at a constant [itex]v[/itex]). This rate of change of momentum per volume [itex]V[/itex] is equal to the force on the plate [itex]F_{\textrm{plate}}[/itex] per unit volume because inside this control volume, the flow is decelerated to zero x-velocity (or whatever direction you choose to be normal to the plate).

So the next step is to look at [itex]\frac{d \rho}{dt}[/itex].

[tex]\frac{d \rho}{dt} = \frac{1}{V}\frac{d m}{dt} = \frac{1}{V}\rho v A[/tex]

Plugging that back into the original momentum balance gives you

[tex]\frac{1}{V}\rho v^2 A = \frac{F_{\textrm{plate}}}{V}[/tex]

Which simplifies to

[tex]F_{\textrm{plate}} = \rho v^2 A[/tex]
 

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