Fire Service Hydraulics

Chapter 4
Hydraulic Measurement and Calculation Methods

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Hydraulic Measurement and Calculation Methods

Introduction

Fire-service hydraulics converts observations—pressure, flow, elevation and pipe dimensions—into decisions about water supply and fire attack. A firefighter may need to determine whether a hydrant can supply an appliance, whether a pump is producing the required discharge pressure, whether a nozzle is flowing correctly, or whether a pressure loss is caused by friction, elevation or equipment.

Reliable measurement is therefore as important as the equation used. A pressure gauge that is not zeroed, a pitot tube held at the wrong angle, or a flow meter installed in disturbed flow can produce a result that appears precise but is operationally unsafe. This chapter presents the principal instruments and calculation methods used in fire-service water-supply assessment.

Learning Objectives

By the end of this chapter, the learner should be able to:

  1. distinguish static, residual, discharge and stagnation pressure;
  2. select and use pressure gauges, flow meters, pitot tubes and hydrant-test equipment;
  3. calculate area, velocity, discharge and nozzle flow using consistent units;
  4. apply Bernoulli’s equation and practical friction-loss relationships;
  5. prepare and interpret a hydraulic worksheet;
  6. identify measurement errors, limitations and safety requirements; and
  7. evaluate a hydrant or water-supply test for fire-service use.

1. Fundamental Hydraulic Quantities

1.1 Pressure

Pressure is force per unit area:

p = F ÷ A

where p is pressure, F is force normal to a surface, and A is area. In SI units, pressure is measured in pascals (Pa), commonly kilopascals (kPa) or bar. Fire-service instruments may also use pounds per square inch (psi).

Useful conversions are:

  • 1 bar = 100 kPa approximately;
  • 1 psi = 6.895 kPa approximately;
  • 1 metre of water head = 9.81 kPa approximately;
  • 1 psi = 0.703 m of water head approximately.

Static pressure is the pressure when water is not flowing. Residual pressure is the pressure remaining at a point while a specified flow is being discharged. Residual pressure is usually more useful than static pressure because it indicates the supply’s behaviour under demand.

A gauge measures pressure relative to its reference. A gauge reading of zero does not necessarily mean zero absolute pressure; it means the measured pressure is equal to atmospheric pressure. This distinction matters when using gas laws, cavitation analysis or absolute-pressure instruments, but ordinary fire-ground pressure calculations normally use gauge pressure.

1.2 Head and elevation

Pressure may be expressed as energy per unit weight, called pressure head:

hp = p ÷ (ρg)

where hₚ is pressure head in metres of water, p is pressure in pascals, ρ is water density in kg/m³, and g is gravitational acceleration, approximately 9.81 m/s².

For water, an increase in elevation reduces available pressure. The elevation-pressure relationship is:

∆pe = ρg∆z

where ∆z is the vertical rise. In practical terms, a rise of 10 m requires approximately 98.1 kPa, or 1 bar, of pressure before friction losses are considered.

1.3 Flow rate, velocity and discharge

Volumetric flow rate, or discharge, is the volume passing a section per unit time. It is represented by Q and measured in m³/s, L/min, L/s, or gallons per minute (gpm).

The continuity equation is:

Q = Av

where A is cross-sectional area in m² and v is mean velocity in m/s. For a circular hose or pipe:

A = πD² ÷ 4

where D is internal diameter in metres. The diameter must be the actual internal diameter, not the nominal trade size.

Example 1: Discharge from a hose

A hose has an internal diameter of 65 mm and carries water at an average velocity of 3.0 m/s. Find the discharge.

Convert diameter: D = 0.065 m.

A = π(0.065)² ÷ 4 = 0.00332 m²
Q = 0.00332 × 3.0 = 0.00996 m³/s

Since 1 m³/s = 1,000 L/s, the discharge is approximately 9.96 L/s, or 598 L/min.

2. Pressure Measurement Equipment

2.1 Bourdon-tube pressure gauges

The common fire-service gauge uses a curved elastic Bourdon tube. Internal pressure tends to straighten the tube, and mechanical linkage moves a pointer across a calibrated dial. Gauges may be compound gauges, suction gauges, discharge gauges or test gauges.

A gauge should be selected so that normal readings lie near the middle of its scale. A 0–25 bar gauge is less useful for accurately reading a normal 2 bar residual pressure than a suitable low-range gauge. The gauge should also be rated for the expected pressure, temperature, vibration and water-hammer conditions.

Before use, the operator should:

  • inspect the lens, pointer, connection and seal;
  • confirm that the pointer returns to zero when depressurised;
  • verify the calibration status;
  • open valves gradually; and
  • avoid striking or dropping the instrument.

Gauge error may be caused by mechanical damage, blocked snubbers, temperature, pulsating flow or an incorrect scale. A gauge reading should be recorded with its location, units, time and operating condition.

2.2 Pressure transducers and digital instruments

Electronic transducers convert pressure into an electrical signal. They can record rapidly changing pressures and transmit values to a data logger or pump-control system. Their advantages include automatic recording and remote display. Their limitations include battery failure, calibration drift, electrical damage and sensitivity to incorrect zeroing.

Digital indication does not guarantee accuracy. A digital gauge with a resolution of 0.01 bar may still have an accuracy error of ±0.1 bar. Resolution and accuracy are different properties.

2.3 Pressure-test points

Pressure should be measured at the point relevant to the decision. For example, pump discharge pressure does not necessarily equal nozzle pressure because hose, appliance and elevation losses occur between the pump and nozzle. Test points should be securely connected, free of leaks and positioned so that trapped air does not distort the reading.

3. Flow-Meter Measurement

A flow meter measures discharge directly or infers it from another physical quantity. Common types include turbine meters, electromagnetic meters, ultrasonic meters and differential-pressure meters.

InstrumentMeasurement principleStrengthImportant limitation
Turbine meterRotor speed related to flowPortable and responsiveMoving parts and minimum-flow limits
Electromagnetic meterVoltage induced by conductive waterNo obstruction and good accuracyRequires power and conductive liquid
Ultrasonic meterTransit-time or Doppler shiftCan be externally mountedSensitive to installation and pipe condition
Differential-pressure meterPressure difference across a restrictionRobust and establishedCauses permanent or recoverable pressure loss

Flow-meter installation requires attention to straight pipe length, full-pipe conditions, air entrainment, sediment and the manufacturer’s calibration requirements. A meter installed immediately downstream of an elbow, partially filled pipe or rapidly changing valve may not provide a dependable result.

When a flow meter is used in a hydrant test, the operator should record the meter location and whether the reading represents the total flow from the hydrant or only one outlet. The meter should be selected for the expected range; operation far below or above its calibrated range reduces confidence.

4. Pitot Tubes and Hydrant Test Equipment

4.1 Pitot-tube principle

A pitot tube measures stagnation pressure at the tip of a probe. The moving water is brought nearly to rest at the opening, converting velocity energy into pressure. The velocity relationship is:

v = Cp √(2∆p ÷ ρ)

where v is local velocity in m/s, Cₚ is the pitot coefficient, ∆p is the measured velocity pressure in Pa, and ρ is water density in kg/m³. For a properly shaped and calibrated pitot tube, Cₚ is often close to 1.0, but the manufacturer’s value should be used.

The equation assumes incompressible flow, a correctly aligned probe and a valid velocity-pressure reading. It measures local velocity, not automatically the average velocity across an irregular outlet. In hydrant testing, the standard discharge relationship supplied by the equipment manufacturer or applicable standard should be followed.

For a nozzle of diameter d discharging to atmosphere, the general equation is:

Q = Cd A √(2∆p ÷ ρ)

where C_d is the discharge coefficient, A is nozzle area, ∆p is pressure difference between the nozzle interior and the receiving atmosphere, and ρ is water density. The equation is applicable when the nozzle geometry and discharge conditions are stable and the coefficient is appropriate.

For a circular nozzle, A = πd² ÷ 4. In common US customary fire-service practice, a smooth-bore nozzle is often estimated by:

Q ≈ 29.84d²√P

where Q is gpm, d is nozzle diameter in inches and P is nozzle pressure in psi. The coefficient is not universal: nozzle shape, coefficient of discharge and units determine the appropriate constant.

4.2 Pitot-tube procedure

A typical hydrant-flow test involves attaching a calibrated playpipe or test cap, opening the hydrant slowly, allowing the flow to stabilise and placing the pitot tube at the specified position. The probe should face the flow and be held at the prescribed distance from the outlet. The operator records static pressure before opening the outlet, then residual pressure and pitot pressure while flowing.

The operator must stand clear of the outlet and reaction forces. The outlet should not be blocked by hands, loose equipment or an improperly secured cap. Water discharge should be directed away from traffic, electrical equipment, pedestrians and structures.

4.3 Hydrant-test data

A basic test record includes:

  • hydrant identification and location;
  • date, time and weather conditions;
  • static pressure;
  • residual pressure at the flowing hydrant;
  • flow pressure or pitot reading;
  • outlet size and test equipment;
  • number of outlets opened;
  • elevation information;
  • instrument identification and calibration status; and
  • observations such as vibration, discolouration or leakage.

5. Energy Relationships and Pressure Loss

5.1 Bernoulli equation

For steady, incompressible flow along a streamline, the extended Bernoulli equation is:

p₁ ÷ (ρg) + z₁ + α₁v₁² ÷ (2g) + Hp = p₂ ÷ (ρg) + z₂ + α₂v₂² ÷ (2g) + hL

Here p is pressure, z is elevation, v is mean velocity, α is the kinetic-energy correction factor, Hₚ is pump head added, and hL is total head loss. Subscripts 1 and 2 identify two locations. For many fire-service calculations, velocity correction factors are approximated as 1, but the equation still requires that friction and fitting losses be considered.

Total loss may be represented as:

hL = hf + hm

where h_f is major friction loss in straight pipe or hose and h_m is minor loss through fittings, valves, appliances and entrances or exits. “Minor” does not mean unimportant; several fittings may produce a substantial combined loss.

5.2 Darcy–Weisbach equation

The general friction-loss equation is:

hf = f(L ÷ D)(v² ÷ 2g)

where f is the Darcy friction factor, L is pipe length, D is internal diameter, v is mean velocity and g is gravitational acceleration. The friction factor depends on Reynolds number and relative roughness. This method is widely applicable but requires suitable values of f.

For a fitting or appliance:

hm = K(v² ÷ 2g)

where K is the dimensionless loss coefficient for that component. Manufacturer data or accepted tables should be used rather than guessed values.

5.3 Hazen–Williams relationship

The Hazen–Williams equation is widely used for water in fire-protection piping. In SI form, one commonly used expression for head loss is:

hf = 10.67LQ1.852 ÷ (C1.852D4.87)

where h_f is head loss in metres of water, L is pipe length in metres, Q is flow in m³/s, D is internal diameter in metres and C is the Hazen–Williams roughness coefficient. The equation is empirical and intended primarily for water in full pipes under ordinary engineering conditions. Its coefficient and constant must match the chosen unit system.

Hazen–Williams should not be used blindly for unusual fluids, highly transient flows or conditions outside the range for which the selected coefficient is appropriate. Fire-service worksheets should identify whether Darcy–Weisbach or Hazen–Williams has been used.

5.4 Equivalent length and appliance loss

A fitting can be represented by an equivalent length of straight pipe, or its loss can be calculated directly with a K value. Equivalent-length methods are convenient for worksheets but depend on pipe diameter, roughness and flow conditions. Appliance loss should preferably come from tested manufacturer data.

6. Worked Calculations

Example 2: Velocity from pitot pressure

A pitot tube measures 12 kPa velocity pressure in water. Assume Cₚ = 1.00 and ρ = 1,000 kg/m³. Find local velocity.

Convert 12 kPa to 12,000 Pa:

v = 1.00√(2 × 12,000 ÷ 1,000)
v = √24 = 4.90 m/s

The result is local velocity at the probe, not necessarily the average velocity through the entire outlet.

Example 3: Smooth-bore nozzle discharge

A 19 mm smooth-bore nozzle operates at 700 kPa. Estimate discharge using C_d = 0.98 and water density of 1,000 kg/m³.

Nozzle diameter: d = 0.019 m.

A = π(0.019)² ÷ 4 = 0.0002835 m²
Q = 0.98 × 0.0002835 × √(2 × 700,000 ÷ 1,000)
Q = 0.0002778 × 37.42 = 0.01039 m³/s

Thus, Q ≈ 10.4 L/s, or approximately 624 L/min.

Example 4: Pressure requirement including elevation

A pump supplies a nozzle 18 m above the pump. The required nozzle pressure is 500 kPa, and calculated friction and appliance losses total 180 kPa. Neglect velocity-head differences. Find the approximate pump discharge pressure.

Elevation loss:

∆pe = ρg∆z = 1,000 × 9.81 × 18 = 176,580 Pa ≈ 176.6 kPa

Required pump pressure:

ppump = 500 + 180 + 176.6 = 856.6 kPa

The pump should therefore provide approximately 857 kPa at the relevant operating flow, subject to the actual pump, hose and appliance characteristics.

7. Hydraulic Worksheets and Field Interpretation

A hydraulic worksheet should make the calculation traceable. A practical format is:

ItemSymbolValueUnitSource or assumption
Flow demandQ10.4L/sNozzle calculation
Hose internal diameterD0.065mManufacturer data
Hose lengthL60mMeasured route
Elevation rise∆z18mSite survey
Nozzle pressurepₙ500kPaOperational requirement
Friction lossh_f—kPaApproved method
Appliance lossh_m—kPaManufacturer data
Required pump pressurepₚ—kPaSum of requirements

The worksheet should distinguish measured data from assumptions. It should also show whether pressure is gauge or absolute, whether flow is total or per line, and whether losses are stated as pressure or head.

A useful pressure balance is:

ppump = pnozzle + pelevation + pfriction + pappliances ± pvelocity

The velocity-pressure term is included only when the change in velocity head is relevant. It should not be added automatically as a duplicate of friction loss.

When interpreting a hydrant test:

  • high static pressure with a large drop during flow may indicate limited supply capacity, undersized mains or upstream restriction;
  • low static and low residual pressure may indicate a weak supply, elevation disadvantage or a closed or restricted valve;
  • stable residual pressure with increasing flow generally indicates useful available capacity, but the actual demand must be compared with the required flow;
  • a sudden fluctuation may indicate air, water hammer, pump interaction, valve movement or unstable measurement.

A single hydrant test describes conditions at one time. It does not prove performance during every season, simultaneous demand, system failure or firefighting incident.

8. Available Flow and Extrapolation

The available flow at a hydrant depends on the residual pressure that can be accepted by the system. A simple field comparison is to record static pressure, flow rate and residual pressure. If the tested flow produces a residual pressure below the operational minimum, the test demand is greater than the acceptable available flow under those conditions.

For a rough system estimate, the relationship between pressure drop and flow is often represented as:

∆p = kQn

where k is a system coefficient and n depends on the adopted hydraulic model. This relationship should not be treated as a universal law. It is a fitted approximation for a defined pipe network and range of conditions. Extrapolation far beyond the tested flow can be misleading, particularly where pumps, pressure-reducing devices, storage levels or control valves influence performance.

The most defensible procedure is to use approved hydraulic software, network data or multiple test points when a design decision is significant. Field estimation is suitable for operational awareness but should not replace formal design verification.

9. Illustrative Case: Industrial Hydrant Assessment

Background

A training facility has a hydrant located near a warehouse. The incident plan requires 10 L/s at the attack appliance. The nozzle is 18 m above the pump appliance. The measured static hydrant pressure is 620 kPa. During a controlled test, 8 L/s is discharged and residual pressure is 410 kPa.

Problem

The officer must determine whether the hydrant test provides evidence that the required flow can be supported while maintaining a practical residual pressure.

Analysis

The test demonstrates that 8 L/s is available at 410 kPa residual pressure under the test conditions. However, it does not directly prove that 10 L/s will be available. The officer should examine the pressure-flow trend, hydrant size, main size, elevation, simultaneous demands and the minimum residual pressure required by the system owner.

If the required nozzle pressure is 500 kPa and estimated downstream losses are 180 kPa, the elevation requirement for 18 m is approximately 177 kPa. The total downstream requirement is therefore approximately:

500 + 180 + 177 = 857 kPa

This pressure must be produced at the pump, not necessarily at the hydrant. The hydrant’s residual pressure of 410 kPa cannot simply be added to nozzle pressure; the system arrangement and pump location must be analysed.

Approach and solution

The crew repeats the test using calibrated equipment, confirms the hydrant elevation and identifies the supply main. A second flow point is obtained, for example 6 L/s, while recording residual pressure. The results are entered into a hydraulic worksheet and reviewed against the water authority’s minimum residual-pressure requirement. If the available supply is inadequate, possible measures include using a closer hydrant, reducing simultaneous demand, deploying a relay supply, using a portable pump or obtaining a formal water-supply assessment.

Outcome

The original test is judged useful but insufficient for approving the full operational plan. A verified supply assessment and a contingency arrangement are added to the pre-incident plan.

Learning points

  1. Static pressure alone is not a capacity measurement.
  2. A test flow is evidence at that flow, not proof of unlimited supply.
  3. Pressure, flow, elevation and losses must be connected in one system model.
  4. Instrument calibration and test documentation affect operational confidence.
  5. A conservative contingency is appropriate when uncertainty may affect life safety.

10. Errors, Limitations and Safe Practice

Common sources of error include incorrect internal diameter, mixed units, reading a gauge while the flow is changing, using a nominal rather than actual nozzle diameter, ignoring elevation, applying the wrong discharge coefficient and extrapolating from one test point.

Other limitations include temperature-dependent water density, air entrainment, partially opened valves, clogged strainers, damaged hydrant barrels, non-uniform outlet geometry and unrecorded simultaneous consumption. Fire pumps may also have different performance at different speeds, suction conditions and discharge pressures.

Safety controls are essential. Hydrant caps and test devices must be secured before pressurisation. Valves should be operated slowly to reduce water hammer. Personnel should remain outside the trajectory of outlets and hoses. Discharge water must be controlled to prevent flooding, erosion, electrical hazards and traffic incidents. Testing should follow the authority having jurisdiction, water-utility requirements, applicable fire-service standards and the equipment manufacturer’s instructions.

11. Technology and Contemporary Practice

Modern systems increasingly use electronic pressure sensors, wireless data logging, integrated pump controls, geographic information systems and hydraulic modelling software. These tools improve trend analysis and enable comparison of tests across time and locations. They do not remove the need for field verification.

Artificial intelligence can assist with anomaly detection, maintenance prioritisation and prediction of hydrant performance from historical records. However, AI output must be treated as decision support. The underlying measurements, calibration records, model assumptions and uncertainty must remain visible to the responsible professional. A safety-critical decision should never rely on an unexplained algorithmic recommendation.

Best-Practice Checklist

Before accepting a hydraulic measurement:

  • confirm the instrument range, units and calibration;
  • inspect connections, seals, valves and hoses;
  • identify the exact measurement point;
  • record static and residual conditions separately;
  • measure or verify actual internal diameters;
  • use consistent units throughout the worksheet;
  • include elevation, friction and appliance losses;
  • state coefficients and assumptions;
  • repeat unusual or unstable measurements; and
  • document conditions sufficiently for another competent person to reproduce the calculation.

Chapter Summary

Hydraulic measurement provides the factual basis for fire-service water-supply decisions. Pressure gauges measure pressure at a point, while flow meters and pitot tubes determine discharge directly or through velocity relationships. The continuity equation links discharge, area and velocity. Nozzle flow is determined from pressure, area, density and a discharge coefficient. Bernoulli’s equation provides the energy framework for combining pressure, elevation, velocity, pump head and losses. Darcy–Weisbach and Hazen–Williams are important friction-loss methods, but their assumptions, coefficients and units must be controlled.

A sound hydraulic worksheet separates measurements from assumptions and accounts for elevation, friction, fittings and appliances. Hydrant tests must record static pressure, residual pressure, flow and equipment details. Static pressure alone cannot establish available flow, and one test point should not be extrapolated carelessly. Accurate instruments, safe procedures, calibrated equipment, documented calculations and conservative professional judgement are essential because hydraulic errors can directly affect fire attack, personnel safety and life protection.

Key Terms

Pressure: Force exerted per unit area.

Static pressure: Pressure measured when water is not flowing.

Residual pressure: Pressure remaining at a point while water is flowing.

Gauge pressure: Pressure measured relative to atmospheric pressure.

Pressure head: Pressure expressed as an equivalent height of water.

Discharge: Volumetric flow rate, represented by Q.

Velocity: Mean speed of water through a cross-sectional area.

Continuity equation: Relationship Q = Av for steady flow.

Pitot tube: Instrument that measures stagnation or velocity pressure.

Velocity pressure: Pressure associated with the motion of flowing water.

Flow meter: Instrument that measures or infers volumetric flow rate.

Discharge coefficient: Factor accounting for non-ideal nozzle or orifice behaviour.

Bernoulli equation: Energy relationship among pressure, elevation, velocity, pump head and losses.

Friction loss: Energy loss caused by resistance in hose or pipe.

Minor loss: Loss caused by fittings, valves, appliances and entrances or exits.

Darcy–Weisbach equation: General friction-loss equation using a friction factor.

Hazen–Williams equation: Empirical water-flow friction-loss relationship.

Hydraulic worksheet: Structured record of measurements, assumptions and calculations.

Water hammer: Pressure surge caused by rapid change in flow.

Available flow: Flow that can be supplied while maintaining specified system conditions.

Review Questions

Short Answer Questions

  1. Distinguish between static pressure and residual pressure.
  2. State the continuity equation and define its variables.
  3. Why must actual internal diameter be used in flow calculations?
  4. What does a pitot tube measure?
  5. Identify four items that should be recorded during a hydrant test.

Long Answer Questions

  1. Explain the operating principles, advantages and limitations of Bourdon-tube gauges, electronic pressure transducers and flow meters.
  2. Describe a safe and technically reliable procedure for conducting a hydrant flow test with a pitot tube.
  3. Explain how pressure, elevation, friction loss and appliance loss are combined using the extended Bernoulli relationship.
  4. Compare Darcy–Weisbach and Hazen–Williams friction-loss methods, including their assumptions and practical uses.
  5. Discuss why a static hydrant-pressure reading cannot by itself establish available fire flow.

Analytical / Application Questions

  1. A 75 mm hose has an internal diameter of 0.075 m and carries water at 2.5 m/s. Calculate its discharge in m³/s and L/min.
  2. A nozzle requires 450 kPa at an elevation 12 m above the pump. Friction and appliance losses are estimated at 140 kPa. Calculate the minimum approximate pump pressure, neglecting velocity-head differences.
  3. A hydrant has a static pressure of 700 kPa and a residual pressure of 360 kPa while flowing 9 L/s. Analyse what additional information is required before deciding whether the hydrant can support a 12 L/s fire attack demand.

Multiple Choice Questions with Answers

Question 1

Which pressure is measured while water is flowing from a hydrant?

A. Static pressure

B. Residual pressure

C. Atmospheric pressure

D. Vapour pressure

Correct Answer: B. Residual pressure

Question 2

The continuity relationship for incompressible flow is Q = Av. What does A represent?

A. Pressure head

B. Pipe length

C. Cross-sectional area

D. Friction factor

Correct Answer: C. Cross-sectional area

Question 3

A circular pipe has an internal diameter of 0.10 m. Its cross-sectional area is approximately:

A. 0.00314 m²

B. 0.00785 m²

C. 0.0314 m²

D. 0.0785 m²

Correct Answer: B. 0.00785 m²

Question 4

A pitot tube primarily measures:

A. Elevation head

B. Velocity or stagnation pressure

C. Water temperature only

D. Pipe roughness directly

Correct Answer: B. Velocity or stagnation pressure

Question 5

Using v = √(2∆p ÷ ρ), what is the velocity for a 2,000 Pa velocity pressure in water of density 1,000 kg/m³, assuming a coefficient of 1.0?

A. 1.0 m/s

B. 2.0 m/s

C. 4.0 m/s

D. 20 m/s

Correct Answer: B. 2.0 m/s

Question 6

Approximately how much pressure is required to overcome a 10 m rise in water elevation?

A. 9.81 kPa

B. 49.1 kPa

C. 98.1 kPa

D. 981 kPa

Correct Answer: C. 98.1 kPa

Question 7

Which equation is a general friction-loss relationship involving Darcy friction factor?

A. Q = Av

B. p = F ÷ A

C. hf = f(L ÷ D)(v² ÷ 2g)

D. ∆p = ρg∆z

Correct Answer: C. hf = f(L ÷ D)(v² ÷ 2g)

Question 8

A nozzle discharge coefficient is used mainly to account for:

A. Elevation above sea level

B. Non-ideal flow behaviour through the nozzle

C. The colour of the hose

D. Atmospheric humidity

Correct Answer: B. Non-ideal flow behaviour through the nozzle

Question 9

Which statement about static hydrant pressure is correct?

A. It alone establishes available flow

B. It is measured only after maximum flow is reached

C. It is measured when the hydrant is not flowing

D. It is identical to nozzle pressure in every system

Correct Answer: C. It is measured when the hydrant is not flowing

Question 10

A sound hydraulic worksheet should clearly distinguish between:

A. Measured data and assumptions

B. Day and night operations only

C. Uniform and decorative labels

D. Personnel rank and hose colour

Correct Answer: A. Measured data and assumptions

Fire Service Hydraulics
Chapter 4 of 14