Question: In the figure 2 alpha = 6 0 deg 1 ?angled slit and alpha = 2 0 deg with

In the figure 2\alpha = 60\deg

1 ?angled slit and \alpha = 20\deg

with angle of attack

jet flow is shown. The density of the stream is \rho = 1000

kg / ?m3

, ?width b = 30 ?cm. ?and the velocity is U = 0.5 ?m / ?s. ?Way

As you can see, single jet flow until the flow bifurcates,

After the slit, two jets are in flow. Both

fluid velocity at the outlet is U value.

The thickness of the exit arms is indicated on the figure.

(Being \beta b and (1-\beta ) ?b, ?respectively). ?Where 0=\beta =1

varies.

Assuming that the flow is planar, the depth is d = 50 ?cm.

(perpendicular to the plane of the figure) ?and gravity

negligible pressure everywhere atmospheric pressure

Assuming that there is pressure,

a) - ?Calculate the lifting and drag forces.

(for =\beta 0.3.)

b) ?Removing with all values remaining constant

what value must have to have zero power?

SORU 4) (25 puan) - P.U (1-b

SORU 4) (25 puan) - P.U (1-b

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