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6.1 The figure below shows a smooth curved vane attached to a rigid foundation. The jet of water, rectangular in section, 75mm wide and 25mm thick, strike the vane with a velocity of 25m/s. Calculate the vertical and horizontal components of the force exerted on the vane and indicate in which direction these components act. [Horizontal 233.4 N acting from right to left. Vertical 1324.6 N acting downwards] ![]() From the question:
Calculate the total force using the momentum equation:
Body force and pressure force are 0. So force on vane:
6.2 ![]() From the question:
Calculate total force.
Calculate the pressure force p1 = p2 = p = hrg = 3010009.81 = 294.3 kN/m2
There is no body force in the x or y directions.
These forces act on the fluid The resultant force on the fluid is
6.3 ![]() From the question a2 = a3 =2x10-3 m2 u = 15 m/s Apply Bernoulli, Change in height is negligible so z1 = z2 = z3 and pressure is always atmospheric p1= p2 = p3 =0. So u1= u2 = u3 =15 m/s By continuity Q1= Q2 + Q3 u1a1 = u2a2 + u3a3 so a1 = a2 + a3 Put the axes normal to the plate, as we know that the resultant force is normal to the plate. Q1 = a1u = 210-315 = 0.03 Q1 = (a2 + a3) u Q2 = a2u Q3 = (a1 - a2)u Calculate total force.
Component in direction of jet = 390 sin
60 = 338 N As there is no force parallel to the plate Fty = 0
Thus 3/4 of the jet goes up, 1/4 down 6.4 ![]() From the question, djet = 0.075m u1=25m/s Q = 25p(0.075/2)2 = 0.11 m3/s Force normal to plate is FTx = rQ( 0 - u1x ) FTx = 10000.11 ( 0 - 25 cos 30 ) = 2.39 kN 6.5 ![]() 1&2 Draw the control volume and the
axis system p1 = 100 kN/m2, Q = 0.3 m3/s q = 45 d1 = 0.15 m d2 = 0.3 m A1 = 0.177 m2 A2
= 0.0707 m2 3 Calculate the total force in the x direction
by continuity
and in the y-direction
4 Calculate the pressure force.
We know pressure at the inlet but not at the outlet. we can use Bernoulli to calculate this
unknown pressure.
where hf is the friction loss In the question it says this can be ignored, hf=0 The height of the pipe at the outlet is 1m above the inlet. Taking the inlet level as the datum: z1 = 0 z2 = 1m So the Bernoulli equation becomes:
5 Calculate the body force The only body force is the force due to gravity. That is the weight acting in the y direction.
There are no body forces in the x direction,
6 Calculate the resultant force
And the resultant force on the fluid is given by
And the direction of application is
The force on the bend is the same magnitude but in the opposite direction
6.6 ![]() From the question, djet = 0.025m FTx = 650 N Force normal to plate is FTx = rQ( 0 - u1x ) 650 = 1000Q ( 0 - u ) Q = au = (pd2/4)u 650 = -1000au2 = -1000Q2/a 650 = -1000Q2/(p0.0252/4) Q = 0.018m3/s 6.7 ![]() From the question:
Calculate the total force using the momentum equation:
Body force and pressure force are 0. So force on vane:
6.8 ![]() 1&2 Draw the control volume and the
axis system p1 = 1.45105 N/m2, Q = 0.45 m3/s q = 45 d1 = 0.6 m d2 = 0.3 m A1 = 0.283 m2 A2
= 0.0707 m2 3 Calculate the total force in the x direction
by continuity
and in the y-direction
4 Calculate the pressure force.
We know pressure at the inlet but not at the outlet. we can use Bernoulli to calculate this unknown pressure.
where hf is the friction loss In the question it says this can be ignored, hf=0 Assume the pipe to be horizontal z1 = z2 So the Bernoulli equation becomes:
5 Calculate the body force The only body force is the force due to gravity. There are no body forces in the x or y directions,
6 Calculate the resultant force
And the resultant force on the fluid is given by
And the direction of application is
The force on the bend is the same magnitude but in the opposite direction
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