In the figure 2 alpha = 6 0 deg 1 ?angled slit and
Question:
In the figure alpha deg
?angled slit and alpha deg
with angle of attack
jet flow is shown. The density of the stream is rho
kg ?m
?width b ?cm ?and the velocity is U ?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 beta ?b ?respectively ?Where beta
varies.
Assuming that the flow is planar, the depth is d ?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
b ?Removing with all values remaining constant
what value must have to have zero power?
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