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Chapter 2 • Theory & Derivations

Centrifugal Pumps, Fans and Hydraulic Systems

Comprehensive university textbook unit covering fundamental principles, governing relationships, and engineering applications of Centrifugal Pumps, Fans and Hydraulic Systems.

§2.1 Pump head from pressure and velocity

**Outcome.** Use conservation laws and appropriate reference stations to analyze **pump head from pressure and velocity**; solve a traceable numerical example; expose model limitations; and justify a provisional engineering choice. This is Unit 02, **Centrifugal Pumps, Fans and Hydraulic Systems**.

§2.2 System curves and operating-point intersection

**Outcome.** Use conservation laws and appropriate reference stations to analyze **system curves and operating-point intersection**; solve a traceable numerical example; expose model limitations; and justify a provisional engineering choice. This is Unit 02, **Centrifugal Pumps, Fans and Hydraulic Systems**.

§2.3 Pump efficiency and power

**Outcome.** Use conservation laws and appropriate reference stations to analyze **pump efficiency and power**; solve a traceable numerical example; expose model limitations; and justify a provisional engineering choice. This is Unit 02, **Centrifugal Pumps, Fans and Hydraulic Systems**.

§2.4 Cavitation and NPSH margin

**Outcome.** Use conservation laws and appropriate reference stations to analyze **cavitation and npsh margin**; solve a traceable numerical example; expose model limitations; and justify a provisional engineering choice. This is Unit 02, **Centrifugal Pumps, Fans and Hydraulic Systems**.

§2.5 Fans and compressible ventilation flow

**Outcome.** Use conservation laws and appropriate reference stations to analyze **fans and compressible ventilation flow**; solve a traceable numerical example; expose model limitations; and justify a provisional engineering choice. This is Unit 02, **Centrifugal Pumps, Fans and Hydraulic Systems**.

THREE WORKED QUESTIONS

Step-by-Step Turbomachinery Solutions

Three original questions connect calculations, definitions and interpretation. Open each solution to follow the reasoning.

Solved Problem Example 2.1: Calculation & Verification: Pump head from pressure and velocity

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Pump head from pressure and velocity** under steady operational loading.

Worked Engineering Derivation:

**Teaching case:** For water at 998 kg/m3, 200 kPa pressure rise and negligible elevation or velocity difference give H≈20.43 m. **Explicit substitution:** H = 200,000/(998×9.81); therefore **20.43 m**. This is pressure head only; add velocity and elevation terms if nonzero. Check arithmetic independently. Then perturb one input by 10%: linear, quadratic and cubic factors become 1.1, 1.21 and 1.331, respectively. Recompute nonlinear property relationships. An algebraic change is not evidence of a new real-machine operating point.

Solved Problem Example 2.2: Calculation & Verification: System curves and operating-point intersection

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **System curves and operating-point intersection** under steady operational loading.

Worked Engineering Derivation:

**Teaching case:** A test loop with 12 m static head and K=8000 s2/m5 requires 32 m at Q=0.050 m3/s. **Explicit substitution:** H=12+8000×(0.050)²; therefore **32.0 m**. Square law here assumes the fixed system resistance coefficient remains appropriate. Check arithmetic independently. Then perturb one input by 10%: linear, quadratic and cubic factors become 1.1, 1.21 and 1.331, respectively. Recompute nonlinear property relationships. An algebraic change is not evidence of a new real-machine operating point.

Solved Problem Example 2.3: Calculation & Verification: Pump efficiency and power

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Pump efficiency and power** under steady operational loading.

Worked Engineering Derivation:

**Teaching case:** Water at 1000 kg/m3 and Q=0.035 m3/s over 25 m, with pump eta=0.76 and motor eta=0.93, uses about 12.13 kW. **Explicit substitution:** P = 1000×9.81×0.035×25/(0.76×0.93); therefore **12.13 kW**. Fluid power is 8.584 kW, less than electrical input. Check arithmetic independently. Then perturb one input by 10%: linear, quadratic and cubic factors become 1.1, 1.21 and 1.331, respectively. Recompute nonlinear property relationships. An algebraic change is not evidence of a new real-machine operating point.

Solved Problem Example 2.4: Calculation & Verification: Cavitation and NPSH margin

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Cavitation and NPSH margin** under steady operational loading.

Worked Engineering Derivation:

**Teaching case:** At suction absolute pressure 65 kPa, vapor pressure 3 kPa, rho=1000 kg/m3 and negligible velocity correction, NPSHa≈6.32 m. **Explicit substitution:** NPSHa = (65,000−3,000)/(1000×9.81); therefore **6.32 m**. Absolute suction and vapor pressures must share the same reference. Check arithmetic independently. Then perturb one input by 10%: linear, quadratic and cubic factors become 1.1, 1.21 and 1.331, respectively. Recompute nonlinear property relationships. An algebraic change is not evidence of a new real-machine operating point.

Solved Problem Example 2.5: Calculation & Verification: Fans and compressible ventilation flow

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Fans and compressible ventilation flow** under steady operational loading.

Worked Engineering Derivation:

**Teaching case:** A fan delivering 2.5 m3/s against 800 Pa total-pressure rise gives 2.0 kW air power and 3.08 kW input at overall eta=0.65. **Explicit substitution:** P_air=800×2.5=2000 W; P_input=2000/0.65; therefore **2.00 kW useful; 3.08 kW input**. Static pressure must not be substituted for total pressure without correction. Check arithmetic independently. Then perturb one input by 10%: linear, quadratic and cubic factors become 1.1, 1.21 and 1.331, respectively. Recompute nonlinear property relationships. An algebraic change is not evidence of a new real-machine operating point.