Fluid Dynamics: Energy & Momentum Worked Examples

The solutions separate continuity, energy, and momentum deliberately. Moving-vane examples identify whether the device is a single translating plate or a continuous ideal Pelton runner before selecting a power model.

Problem 1: Bernoulli Flow Through a Horizontal Contraction

Water flows through a horizontal pipe. Section 1 has D1=150 mmD_1=150\text{ mm} and p1=200 kPap_1=200\text{ kPa} gauge; Section 2 has D2=75.0 mmD_2=75.0\text{ mm} and p2=100 kPap_2=100\text{ kPa} gauge. Neglect losses and take kinetic-energy correction factors as one. Determine V1V_1 and discharge.

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Problem 2: Ideal Jet from a Reservoir Nozzle

A 50.0 mm50.0\text{ mm} nozzle discharges water to atmosphere from a large reservoir whose free surface is 5.00 m5.00\text{ m} above the nozzle center. Neglect losses. Determine jet velocity and discharge.

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Problem 3: Pump Head and Shaft Input Power

A pump transfers Q=0.0500 m3/sQ=0.0500\text{ m}^3/\text{s} of water between large reservoirs whose free surfaces differ by 30.0 m30.0\text{ m}. Total pipeline loss is 5.00 m5.00\text{ m} and pump efficiency is 80.0%80.0\%. Determine pump head, water power, and shaft input power.

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Problem 4: Turbine Output from a Reservoir Drop

Water flows at 2.00 m3/s2.00\text{ m}^3/\text{s} from an upper reservoir to a lower reservoir 25.0 m25.0\text{ m} below. Pipeline losses total 3.00 m3.00\text{ m} and turbine efficiency is 85.0%85.0\%. Determine the hydraulic head available at the turbine and output power.

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Problem 5: Absolute Pressure at a Siphon Crest

A siphon crest is 6.00 m6.00\text{ m} above the source-reservoir free surface. Water speed at the crest is 3.00 m/s3.00\text{ m/s}, head loss from the reservoir to the crest is 0.500 m0.500\text{ m}, and atmospheric pressure is 101.3 kPa101.3\text{ kPa} absolute. Determine crest gauge and absolute pressure.

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Problem 6: Pitot-Static Velocity Measurement

A Pitot-static tube in air measures stagnation-minus-static pressure Δp=3.50 kPa\Delta p=3.50\text{ kPa}. Air density is 1.20 kg/m31.20\text{ kg/m}^3. Assuming incompressible behavior and calibration coefficient C=1.00C=1.00, determine local speed.

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Problem 7: Axial Force on a Reducing Nozzle

A horizontal nozzle contracts from D1=100 mmD_1=100\text{ mm} to D2=50.0 mmD_2=50.0\text{ mm}. Water discharge is 0.0200 m3/s0.0200\text{ m}^3/\text{s}, inlet gauge pressure is 200 kPa200\text{ kPa}, and the outlet jet is atmospheric. Neglect weight and wall shear. Determine the force of water on the nozzle.

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Problem 8: Force on a 90-Degree Elbow

A horizontal 150 mm150\text{ mm} elbow turns water from the positive xx direction to the positive yy direction. Q=0.0500 m3/sQ=0.0500\text{ m}^3/\text{s}, p1=150 kPap_1=150\text{ kPa} gauge, and p2=120 kPap_2=120\text{ kPa} gauge. Diameter is constant and weight is neglected. Determine the force of water on the elbow.

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Problem 9: Maximum Power for a Single Moving Flat Plate

A water jet of area A=0.00200 m2A=0.00200\text{ m}^2 and speed V=20.0 m/sV=20.0\text{ m/s} strikes a single flat plate moving away in the jet direction. Neglect gravity and splash momentum in the jet direction. Determine the plate speed for maximum power and the corresponding force and power.

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Problem 10: Ideal Continuous Pelton Bucket Series

An ideal Pelton runner continuously receives a water jet with Q=0.0500 m3/sQ=0.0500\text{ m}^3/\text{s} and V=30.0 m/sV=30.0\text{ m/s}. Assume buckets reverse the relative velocity by 180∘180^\circ without friction and the runner speed is u=15.0 m/su=15.0\text{ m/s}. Determine tangential force and power.

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Problem 11: Venturi Pressure-Head Difference

A horizontal Venturi meter carries water with D1=300 mmD_1=300\text{ mm}, D2=150 mmD_2=150\text{ mm}, discharge Q=0.150 m3/sQ=0.150\text{ m}^3/\text{s}, and Cd=0.980C_d=0.980. Determine the inlet-to-throat piezometric-head difference represented by the standard calibrated relation.

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Problem 12: Stagnation Pressure Increase

Water moves locally at V=6.00 m/sV=6.00\text{ m/s} where static pressure is 120 kPa120\text{ kPa} gauge. At the same elevation, estimate stagnation pressure under steady incompressible, negligible-loss deceleration.

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