Water (density = 1000 kg/m3) flows through a duct that makes a 180 degree U-shaped bend...
Water (density = 1000 kg/m3) flows through a duct that makes a 180 degree U-shaped bend (see below). Assume that the fluid is incompressible through the duct and the velocity at the inlet is V1 = 24 m/s. Assume that the momentum-flux correction factor at both inlet (point 1) and outlet (point 2) is 2.1. The gage pressures are P1 = 120 kPa at the inlet and P2 = 248 kPa at the outlet of the bend. The inlet is 2 m above the outlet. Cross-sectional areas are A1 = 0.02 m2 and A2 = 0.04 m2. What is the force of the duct on the fluid? The weight of the control volume may be ignored.
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Water (density = 1000 kg/m3) flows through a duct
that makes a 180 degree U-shaped bend...
Water flows steadily through a curved duct that turns the flow through angle = 135 degrees,...
Water flows steadily through a curved duct that turns the flow
through angle = 135 degrees, as shown in Fig. 3. The
cross-sectional area of the duct changes from A1 = 0.025 m2 at the
inlet to A2 = 0.05 m2 at the outlet. The average velocity at the
duct inlet is V1 = 6 m/s. The momentum flux correction factor may
be taken as 1 = 1.01 at the duct inlet and 2 = 1.03 at the its
outlet....
Water flows steadily through a curved duct that turns the flow through angle @= 135º, as...
Water flows steadily through a curved duct that turns the flow through angle @= 135º, as shown in Fig. 3. The cross-sectional area of the duct changes from A1 = 0.025 m² at the inlet to A2 = 0.05 m’ at the outlet. The average velocity at the duct inlet is V1 = 6 m/s. The momentum flux correction factor may be taken as B1 = 1.01 at the duct inlet and B2 = 1.03 at the its outlet. The...
asap please, will rate! 3. Water flows steadily through a curved duct that turns the flow...
asap please, will rate!
3. Water flows steadily through a curved duct that turns the flow through angle 0= 135º, as shown in Fig. 3. The cross-sectional area of the duct changes from Aj 0.025 m² at the inlet to A2 = 0.05 m² at the outlet. The average velocity at the duct inlet is V1 = 6 m/s. The momentum flux correction factor may be taken as Bi= 1.01 at the duct inlet and B2 = 1.03 at the...
please help...add sketch Water flows steadily through a curved duct that turns the flow through angle...
please help...add sketch
Water flows steadily through a curved duct that turns the flow through angle = 1359, as shown in Fig. 3. The cross-sectional area of the duct changes from A1 = 0.025 m’ at the inlet to Az = 0.05 m² at the outlet. The average velocity at the duct inlet is V1 = 6 m/s. The momentum flux correction factor may be taken as B - 1.01 at the duct inlet and B = 1.03 at the...
(15 points) Water at 20 °C flows through a 180° pipe bend. Pressures and diameters of...
(15 points) Water at 20 °C flows through a 180° pipe bend. Pressures and diameters of the pipe at point 1 and two are given as P,-350 kPa, D1-30 cm, P., 120 kPa, and D2 . 8 cm. Neglecting the pipe and water weight, answer the following questions. Patm is 100 kPa, and the total reaction force in the x direction, F., is measured as-20 kN. 4. P-100 kP a. What are gage pressures at point 1 and 2 b....
Water flows through a 180 degree reducing bend, as shown. The discharge is 0.25 mA3/s, and...
Water flows through a 180 degree reducing bend, as shown. The discharge is 0.25 mA3/s, and the pressure at the center of the inlet section is 150 kPa gage. If the bend volume is 0.10 mA3, and it is assumed that the Bernoulli equation is valid, what force is required to hold the bend in place? The metal in the bend weighs 500 N. 30 cm - 10 cm 15 cm
Question 2 (a) An incompressible fluid of density ρ and viscosity μ flows through a curved...
Question 2 (a) An incompressible fluid of density ρ and viscosity μ flows through a curved duct that turns the flow through angle θ. (ii) (iii) (i) Write an expression for the horizontal force F of the fluid on the walls of the duct in 4 marks) terms of the given variables (ignore the gravity); Calculate the force Fx, when: θ = 135°, ρ = 9982 kg/m , μ=1.003x10-3 kg/m.s., Al = 0.025 m2, A2-0.05 m, Vi-6 m/s, Plaage-78.47 kPa,...
3. Water flows through a circular channel that has a diameter of d= 75 mm at...
3. Water flows through a circular channel that has a diameter of d= 75 mm at both the inlet and outlet, as shown below. The fluid enters with uniform velocity U = 7.5 m/s. The channel makes a 90° bend that distorts the flow to produce the velocity profile at the outlet described by the function, v(r) = Vmax ( 1 -722 Assume steady, incompressible flow. Density of water is 1000 kg/m² a) Find the value of Vmax. b) Find...
Problem 1 (30): Water (density p 999 kg/m') flows through a pipe bend and constriction as...
Problem 1 (30): Water (density p 999 kg/m') flows through a pipe bend and constriction as shown in the schematic. The pipe section is connected to input and output pipes at loc ations A and B. the inlet point A is located 1 m higher in elevation compared to the exit point B. The total loss d ue to pipe friction, bend, and constriction can be approximated as EU = etY2 with et = 2.1 2 Find the total force...
Show all work and answer all parts of the problem please. The 45 degree elbow nozzle discharges water into the atmosphere. The cross-sectional area of the elbow is 25 cm2 150 cm2 at the inlet and...
Show all work and answer all parts of the problem
please.
The 45 degree elbow nozzle discharges water into the atmosphere. The cross-sectional area of the elbow is 25 cm2 150 cm2 at the inlet and 25 cm2 at the exit. Velocity at point 1 and 2 are given as 2 m/s and 12 m/s 450 respectively. The gage pressure at 1 is 73 kPa 150 em2 30 cm The elevation difference between the centers of the exit and the...
Water flows steadily through a curved duct that turns the flow
through angle = 135 degrees, as shown in Fig. 3. The
cross-sectional area of the duct changes from A1 = 0.025 m2 at the
inlet to A2 = 0.05 m2 at the outlet. The average velocity at the
duct inlet is V1 = 6 m/s. The momentum flux correction factor may
be taken as 1 = 1.01 at the duct inlet and 2 = 1.03 at the its
outlet....
Water flows steadily through a curved duct that turns the flow through angle @= 135º, as shown in Fig. 3. The cross-sectional area of the duct changes from A1 = 0.025 m² at the inlet to A2 = 0.05 m’ at the outlet. The average velocity at the duct inlet is V1 = 6 m/s. The momentum flux correction factor may be taken as B1 = 1.01 at the duct inlet and B2 = 1.03 at the its outlet. The...
asap please, will rate!
3. Water flows steadily through a curved duct that turns the flow through angle 0= 135º, as shown in Fig. 3. The cross-sectional area of the duct changes from Aj 0.025 m² at the inlet to A2 = 0.05 m² at the outlet. The average velocity at the duct inlet is V1 = 6 m/s. The momentum flux correction factor may be taken as Bi= 1.01 at the duct inlet and B2 = 1.03 at the...
please help...add sketch
Water flows steadily through a curved duct that turns the flow through angle = 1359, as shown in Fig. 3. The cross-sectional area of the duct changes from A1 = 0.025 m’ at the inlet to Az = 0.05 m² at the outlet. The average velocity at the duct inlet is V1 = 6 m/s. The momentum flux correction factor may be taken as B - 1.01 at the duct inlet and B = 1.03 at the...
(15 points) Water at 20 °C flows through a 180° pipe bend. Pressures and diameters of the pipe at point 1 and two are given as P,-350 kPa, D1-30 cm, P., 120 kPa, and D2 . 8 cm. Neglecting the pipe and water weight, answer the following questions. Patm is 100 kPa, and the total reaction force in the x direction, F., is measured as-20 kN. 4. P-100 kP a. What are gage pressures at point 1 and 2 b....
Water flows through a 180 degree reducing bend, as shown. The discharge is 0.25 mA3/s, and the pressure at the center of the inlet section is 150 kPa gage. If the bend volume is 0.10 mA3, and it is assumed that the Bernoulli equation is valid, what force is required to hold the bend in place? The metal in the bend weighs 500 N. 30 cm - 10 cm 15 cm
Question 2 (a) An incompressible fluid of density ρ and viscosity μ flows through a curved duct that turns the flow through angle θ. (ii) (iii) (i) Write an expression for the horizontal force F of the fluid on the walls of the duct in 4 marks) terms of the given variables (ignore the gravity); Calculate the force Fx, when: θ = 135°, ρ = 9982 kg/m , μ=1.003x10-3 kg/m.s., Al = 0.025 m2, A2-0.05 m, Vi-6 m/s, Plaage-78.47 kPa,...
3. Water flows through a circular channel that has a diameter of d= 75 mm at both the inlet and outlet, as shown below. The fluid enters with uniform velocity U = 7.5 m/s. The channel makes a 90° bend that distorts the flow to produce the velocity profile at the outlet described by the function, v(r) = Vmax ( 1 -722 Assume steady, incompressible flow. Density of water is 1000 kg/m² a) Find the value of Vmax. b) Find...
Problem 1 (30): Water (density p 999 kg/m') flows through a pipe bend and constriction as shown in the schematic. The pipe section is connected to input and output pipes at loc ations A and B. the inlet point A is located 1 m higher in elevation compared to the exit point B. The total loss d ue to pipe friction, bend, and constriction can be approximated as EU = etY2 with et = 2.1 2 Find the total force...
Show all work and answer all parts of the problem
please.
The 45 degree elbow nozzle discharges water into the atmosphere. The cross-sectional area of the elbow is 25 cm2 150 cm2 at the inlet and 25 cm2 at the exit. Velocity at point 1 and 2 are given as 2 m/s and 12 m/s 450 respectively. The gage pressure at 1 is 73 kPa 150 em2 30 cm The elevation difference between the centers of the exit and the...
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