Hydraulic Learning

Calculating Power Dissipated by Head Loss

Exercise: Power Dissipated by Head Loss

Calculating the Power Dissipated by Head Loss

Context: Energy in Fluid Flow.

When a fluid flows through a pipe, it loses energy due to friction against the walls (major head loss) and obstacles such as elbows, valves, or expansions (minor head loss). This lost energy is converted into heat and must be compensated for, usually by a pump, to maintain the flow. Calculating the power dissipated by this head lossThe reduction in the total head (sum of elevation, pressure, and velocity head) of a fluid as it moves through a pipe system. is therefore a crucial step in designing hydraulic systems.

Pedagogical Note: This exercise will help you master the calculation of different head losses in a simple hydraulic circuit and quantify the energy needed to overcome them, a fundamental skill for any technician or engineer in fluid mechanics.


Learning Objectives

  • Identify and differentiate between major (linear) and minor (singular) head losses.
  • Calculate the flow velocity and the Reynolds number.
  • Determine the friction factor using the Colebrook-White equation.
  • Apply the Darcy-Weisbach formula for major losses.
  • Calculate the sum of minor losses.
  • Determine the hydraulic power (in horsepower) dissipated by the total head loss.

Problem Data

We want to calculate the power dissipated by head loss for a hydraulic circuit transporting water from point A to point B.

Hydraulic Circuit Diagram
A B Elbow 1 Elbow 2 Valve
Parameter Symbol Value Unit
Fluid - Water at 68°F -
Water Specific Weight \(\gamma\) 62.4 lb/ft³
Water Kinematic Viscosity \(\nu\) \(1.06 \times 10^{-5}\) ft²/s
Volume Flow Rate \(Q\) 220 GPM
Inner Pipe Diameter \(D\) 3.94 in
Total Pipe Length \(L\) 656.2 ft
Absolute Pipe Roughness (PVC) \(\varepsilon\) \(5.0 \times 10^{-6}\) ft
Loss Coefficient (90° Elbow) \(K_{\text{elbow}}\) 0.9 -
Loss Coefficient (Valve) \(K_{\text{valve}}\) 0.2 -
Acceleration of Gravity \(g\) 32.2 ft/s²

Questions to Solve

  1. Calculate the flow velocity \(V\) in the pipe.
  2. Calculate the Reynolds number \(Re\).
  3. Determine the friction factor \(f\).
  4. Calculate the major (linear) head loss \(\Delta H_{\text{lin}}\).
  5. Calculate the minor (singular) head loss \(\Delta H_{\text{sing}}\).
  6. Determine the total head loss \(\Delta H_{\text{tot}}\).
  7. Calculate the power \(P\) dissipated by the head loss (in horsepower).

Fundamentals of Head Loss

To solve this exercise, you must master the fundamental formulas for energy loss in pipes.

1. Major (Linear) Head Loss (Darcy-Weisbach)
This is caused by fluid friction along the length of the pipe. The Darcy-Weisbach equation is used to calculate it: \[ \Delta H_{\text{lin}} = f \cdot \frac{L}{D} \cdot \frac{V^2}{2g} \] Where \(f\) is the friction factor, \(L\) is the length, \(D\) is the diameter, \(V\) is the velocity, and \(g\) is the acceleration of gravity.

2. Minor (Singular) Head Loss
These are localized losses caused by pipe fittings (elbows, valves, etc.). They are calculated by summing the effects of each fitting: \[ \Delta H_{\text{sing}} = \left( \sum K_i \right) \cdot \frac{V^2}{2g} \] Where \(K_i\) is the loss coefficient for each component.

3. Dissipated Power (Water Horsepower)
The power lost (dissipated) to friction corresponds to the energy a pump must supply to overcome these losses. In USCS, this is often calculated in horsepower (hp). \[ P \text{ (hp)} = \frac{\gamma \cdot Q \cdot \Delta H_{\text{tot}}}{550} \] Where \(\gamma\) is the specific weight (lb/ft³), \(Q\) is the flow rate in **ft³/s**, \(\Delta H_{\text{tot}}\) is the total head loss in feet, and 550 is the conversion factor (550 ft·lb/s = 1 hp).


Solution: Calculating Power Dissipated by Head Loss

Question 1: Calculate the flow velocity \(V\)

Principle

The fluid velocity is the ratio of the volume flow rate (the volume of fluid passing through a cross-section per unit of time) to the area of that cross-section. It reflects how fast the fluid is moving.

Mini-Lesson

This calculation stems from the principle of conservation of mass for an incompressible fluid. The mass flow rate (\(\dot{m} = \rho \cdot Q\)) is constant. Since \(\rho\) is constant, the volume flow rate \(Q = A \cdot V\) is also constant. Velocity is therefore inversely proportional to the cross-sectional area.

Pedagogical Note

The first step in any USCS hydraulics calculation is to ensure all units are consistent. We must convert Gallons per Minute (GPM) to ft³/s and inches to feet before applying the formulas.

Standards

Common conversions in USCS are: 1 ft³ ≈ 7.48 gallons, and 1 ft = 12 inches. These are essential for all calculations.

Formula(s)

Velocity Formula

\[ V = \frac{Q}{A} \]

Area of a circular cross-section

\[ A = \frac{\pi D^2}{4} \]
Assumptions

We assume the fluid completely fills the pipe and the velocity is uniform across the cross-section (average velocity). In reality, the velocity is zero at the wall and maximum at the center (velocity profile).

Given Data
ParameterSymbolValueUnit
Volume Flow RateQ220GPM
DiameterD3.94in
Tips

For standard domestic or industrial water systems, flow velocity is often between 3 and 10 ft/s. A result far outside this range should alert you to a possible calculation error.

Diagram (Before Calculation)
Pipe Cross-Section and Flow Rate
DQ, V
Calculation(s)

1. Unit Conversion (to ft and s)

We convert the flow rate \(Q\) from GPM to ft³/s and the diameter \(D\) from inches to feet.

\[ \begin{aligned} Q &= 220 \, \frac{\text{gal}}{\text{min}} \cdot \left( \frac{1 \text{ ft}^3}{7.48 \text{ gal}} \right) \cdot \left( \frac{1 \text{ min}}{60 \text{ s}} \right) \approx 0.490 \, \text{ft}^3/\text{s} \\ D &= 3.94 \, \text{in} \div 12 \, \frac{\text{in}}{\text{ft}} \approx 0.328 \, \text{ft} \end{aligned} \]

We now have our flow rate in ft³/s and our diameter in ft, ready for calculations.

2. Area Calculation (A)

We apply the area formula \(A = \frac{\pi D^2}{4}\) with the diameter in feet:

\[ \begin{aligned} A &= \frac{\pi \cdot (0.328 \, \text{ft})^2}{4} \\ A &= \frac{\pi \cdot 0.1076 \, \text{ft}^2}{4} \\ A &\approx 0.0845 \, \text{ft}^2 \end{aligned} \]

The cross-sectional area of our pipe is approximately 0.0845 square feet.

3. Velocity Calculation (V)

We apply the formula \(V = \frac{Q}{A}\) by substituting the converted values:

\[ \begin{aligned} V &= \frac{Q}{A} = \frac{0.490 \, \text{ft}^3/\text{s}}{0.0845 \, \text{ft}^2} \\ V &\approx 5.80 \, \text{ft/s} \end{aligned} \]

The final result for the average flow velocity is 5.80 ft/s.

Diagram (After Calculation)
Visualization of Velocity in the Pipe
V = 5.80 ft/s
Reflections

A velocity of 5.80 ft/s is a very plausible value for a pumping application, ensuring a good trade-off between reasonable head loss and an economical pipe diameter.

Caution

The most common error is mismatching units. Do not divide GPM by area in square inches! All units for primary equations (like \(V=Q/A\)) must be consistent (e.g., feet and seconds).

Key Takeaways

The fundamental relationship between flow rate, velocity, and area is key. Mastering unit conversions (GPM to ft³/s, inches to ft) is non-negotiable.

FAQ
Final Result
The flow velocity in the pipe is approximately 5.80 ft/s.
Your Turn

If the flow rate were 300 GPM with the same diameter, what would the new velocity be?
Hint: Velocity is directly proportional to the flow rate.

Question 2: Calculate the Reynolds number \(Re\)

Principle

The Reynolds number compares the magnitude of inertial forces (which tend to create turbulence) to that of viscous forces (which tend to dampen disturbances and maintain a smooth flow). It is the universal criterion for defining whether a flow is laminar or turbulent.

Mini-Lesson

A flow is said to be:
Laminar (\(Re < 2000\)): Fluid particles slide past one another in orderly layers. Head loss is low.
Transitional (\(2000 < Re < 4000\)): An unstable regime, difficult to predict.
Turbulent (\(Re > 4000\)): The flow is chaotic, with eddies that significantly increase energy loss due to friction.

Pedagogical Note

Determining the flow regime is a mandatory step before you can choose the correct method for calculating the friction factor \(f\). Never skip this step!

Standards

The thresholds of 2000 and 4000 are empirically derived values universally recognized in fluid engineering codes and standards for internal flow in circular pipes.

Formula(s)

Reynolds Number Formula

\[ Re = \frac{V \cdot D}{\nu} \]
Assumptions

We assume the fluid properties (\(\nu\)) are constant. In reality, viscosity depends on temperature, which can vary along the pipe.

Given Data
ParameterSymbolValueUnit
VelocityV5.80ft/s
DiameterD0.328ft
Kinematic Viscosity\(\nu\)1.06 x 10⁻⁵ft²/s
Tips

For water at room temperature in pipes a few inches in diameter, the flow becomes turbulent at very low velocities. In practice, most water applications are turbulent.

Diagram (Before Calculation)
Visualization of Flow Regimes
LaminarTurbulent
Calculation(s)

We apply the Reynolds number formula \( Re = \frac{V \cdot D}{\nu} \) using our consistent set of units (feet and seconds):

\[ \begin{aligned} Re &= \frac{V \cdot D}{\nu} \\ Re &= \frac{5.80 \, \text{ft/s} \cdot 0.328 \, \text{ft}}{1.06 \times 10^{-5} \, \text{ft}^2/\text{s}} \\ Re &= \frac{1.9024}{1.06 \times 10^{-5}} \\ Re &\approx 179,500 \end{aligned} \]

The Reynolds number is 179,500. Since this value is much greater than 4000, we confirm that the flow is turbulent.

Diagram (After Calculation)
Position on the Reynolds Scale
Laminar< 2000Transitional< 4000TurbulentRe=179,500
Reflections

With a value of 179,500, we are well within the turbulent regime. Inertial forces are 179,500 times more significant than viscous forces. Friction will therefore be significant and will depend on the pipe's roughness.

Caution

Ensure you are using kinematic viscosity (\(\nu\), in ft²/s). If you are given dynamic viscosity (\(\mu\), in lb·s/ft²), the formula changes to \(Re = \rho V D / \mu\), where \(\rho\) is the mass density (in slugs/ft³).

Key Takeaways

The Reynolds number is a prerequisite for calculating head loss. Remember the formula \(Re = VD/\nu\) and the regime change thresholds.

Did You Know?

Osborne Reynolds, an Irish engineer, first visualized the laminar-to-turbulent transition in 1883 by injecting a stream of dye into water flowing in a glass tube. His experiment is still replicated in engineering schools today.

FAQ
Final Result
The Reynolds number is approximately 179,500, indicating a turbulent flow regime.
Your Turn

If we were pumping an oil 5 times more viscous (\(\nu = 5.3 \times 10^{-5}\) ft²/s) at the same velocity, what would the new Reynolds number be?

Question 3: Determine the friction factor \(f\)

Principle

The friction factor \(f\) quantifies the intensity of head loss due to friction. In a turbulent regime, it depends on both the Reynolds number (which characterizes the flow) and the relative roughness of the pipe (which characterizes the wall).

Mini-Lesson

For turbulent flows, the relationship between \(f\), \(Re\), and the relative roughness \(\varepsilon/D\) is described by the Colebrook-White equation. This equation is implicit: the friction factor \(f\) appears on both sides, meaning it cannot be solved for directly. To solve it, we must use a numerical method, typically successive iterations.

Pedagogical Note

Choosing the roughness value \(\varepsilon\) is one of the biggest sources of uncertainty in hydraulic calculations. It depends on the material, its surface condition, and its age (corrosion, deposits). Always use reliable tabulated values.

Standards

Roughness values for various piping materials are provided by industrial standards (e.g., ASME, API) and manufacturers. The Darcy friction factor \(f\) used here is standard in US civil and mechanical engineering.

Formula(s)

Colebrook-White Equation

\[ \frac{1}{\sqrt{f}} = -2 \log_{10} \left( \frac{\varepsilon/D}{3.7} + \frac{2.51}{Re \sqrt{f}} \right) \]
Assumptions

We assume the pipe roughness is uniform along its entire length.

Given Data
ParameterSymbolValueUnit
Absolute Roughness\(\varepsilon\)5.0 x 10⁻⁶ft
DiameterD0.328ft
Reynolds NumberRe179,500-
Tips

To start the iterations, a good initial guess for \(f\) can be obtained from a simplified formula (like one for smooth pipes) or by using a typical value like 0.02.

Diagram (Before Calculation)
Principle of the Moody Diagram
Friction Factor, fReynolds Number, Re (log scale)Relative Roughness, ε/DSmooth pipe...Rough pipe
Calculation(s)

1. Calculate Relative Roughness (\(\varepsilon/D\))

Both values are already in feet, so we can directly compute the dimensionless ratio.

\[ \frac{\varepsilon}{D} = \frac{5.0 \times 10^{-6} \, \text{ft}}{0.328 \, \text{ft}} \approx 1.524 \times 10^{-5} \]

This relative roughness of \(1.524 \times 10^{-5}\) is very low, confirming the pipe is "hydraulically smooth".

2. Iteration 1: Initial Guess

We start with an initial guess, \(f_0 = 0.02\). We plug this into the right-hand side of the Colebrook-White equation.

\[ \begin{aligned} \frac{1}{\sqrt{f_1}} &= -2 \log_{10} \left( \frac{\varepsilon/D}{3.7} + \frac{2.51}{Re \sqrt{f_0}} \right) \\ \frac{1}{\sqrt{f_1}} &= -2 \log_{10} \left( \frac{1.524 \times 10^{-5}}{3.7} + \frac{2.51}{179500 \sqrt{0.02}} \right) \\ \frac{1}{\sqrt{f_1}} &\approx -2 \log_{10} (4.12 \times 10^{-6} + 9.89 \times 10^{-5}) \\ \frac{1}{\sqrt{f_1}} &\approx -2 \log_{10} (1.03 \times 10^{-4}) \\ \frac{1}{\sqrt{f_1}} &\approx 7.97 \\ \Rightarrow f_1 &= \left(\frac{1}{7.97}\right)^2 \approx 0.0157 \end{aligned} \]

Our first guess \(f_0=0.02\) is refined to \(f_1 \approx 0.0157\). We use this new value for the next iteration.

3. Iteration 2: Refinement

We plug \(f_1 = 0.0157\) back into the equation.

\[ \begin{aligned} \frac{1}{\sqrt{f_2}} &= -2 \log_{10} \left( \frac{1.524 \times 10^{-5}}{3.7} + \frac{2.51}{179500 \sqrt{0.0157}} \right) \\ \frac{1}{\sqrt{f_2}} &\approx -2 \log_{10} (4.12 \times 10^{-6} + 1.11 \times 10^{-4}) \\ \frac{1}{\sqrt{f_2}} &\approx -2 \log_{10} (1.151 \times 10^{-4}) \\ \frac{1}{\sqrt{f_2}} &\approx 7.88 \\ \Rightarrow f_2 &= \left(\frac{1}{7.88}\right)^2 \approx 0.0161 \end{aligned} \]

The second iteration gives us \(f_2 \approx 0.0161\).

4. Iteration 3: Convergence

We repeat the process with \(f_2 = 0.0161\).

\[ \begin{aligned} \frac{1}{\sqrt{f_3}} &= -2 \log_{10} \left( \frac{1.524 \times 10^{-5}}{3.7} + \frac{2.51}{179500 \sqrt{0.0161}} \right) \\ \frac{1}{\sqrt{f_3}} &\approx -2 \log_{10} (4.12 \times 10^{-6} + 1.10 \times 10^{-4}) \\ \frac{1}{\sqrt{f_3}} &\approx -2 \log_{10} (1.141 \times 10^{-4}) \\ \frac{1}{\sqrt{f_3}} &\approx 7.88 \\ \Rightarrow f_3 &= \left(\frac{1}{7.88}\right)^2 \approx 0.0161 \end{aligned} \]

The third iteration gives \(f_3 \approx 0.0161\), which is the same as \(f_2\). The calculation has converged.

Diagram (After Calculation)
Reading from the Moody Diagram
fReε/D179,5000.0161Curve ε/D = 1.52e-5
Reflections

The value of 0.0161 is obtained by the reference method (Colebrook-White). Note that the original problem in SI units also yielded \(f=0.0161\). This shows that the friction factor is dimensionless, and as long as the inputs (\(Re\) and \(\varepsilon/D\)) are correct, the result is independent of the unit system.

Caution

Be careful to use the base-10 logarithm (\(\log_{10}\)) and not the natural logarithm (\(\ln\)). This is a common mistake when using calculators.

Key Takeaways

In a turbulent regime, the friction factor depends on \(Re\) and \(\varepsilon/D\). The Colebrook-White equation is the standard for calculating it and is solved by iteration.

Did You Know?

The Moody diagram, which is a graphical plot of the Colebrook-White equation, was the primary tool for solving this for decades before calculators and computers made iteration easy.

FAQ
Final Result
The friction factor, calculated by iteration, is approximately 0.0161.
Your Turn

If the pipe were made of worn cast iron (\(\varepsilon = 0.00164\) ft), what would the new friction factor \(f\) be (keeping \(Re=179,500\))?

Question 4: Calculate the major (linear) head loss \(\Delta H_{\text{lin}}\)

Principle

Linear (or major) head loss represents the "continuous" energy loss due to the fluid's friction against the pipe walls along its entire length. It is often the most significant contribution to the total head loss in long pipelines.

Mini-Lesson

The Darcy-Weisbach formula shows that these losses increase with the square of the velocity. This means that doubling the flow rate (and thus the velocity) approximately quadruples the friction losses. They also increase linearly with length and inversely with diameter.

Pedagogical Note

The unit for \(\Delta H\) is feet. This should be interpreted as a "head" of fluid equivalent to the energy lost. If \(\Delta H = 10\) ft, it means the fluid lost as much energy as if it had fallen from a height of 10 feet.

Standards

The Darcy-Weisbach equation is the international standard for calculating linear head loss in pressurized pipes.

Formula(s)

Darcy-Weisbach Formula

\[ \Delta H_{\text{lin}} = f \cdot \frac{L}{D} \cdot \frac{V^2}{2g} \]
Assumptions

We assume that the diameter, roughness, and flow rate are constant over the entire length \(L\).

Given Data
ParameterSymbolValueUnit
Friction Factorf0.0161-
LengthL656.2ft
DiameterD0.328ft
VelocityV5.80ft/s
Gravityg32.2ft/s²
Tips

The term \(V^2 / (2g)\) is called the "velocity head". It is often useful to calculate it once and reuse it for both linear and singular loss calculations.

Diagram (Before Calculation)
Representation of a Straight Pipe
Length L = 656.2 ft
Calculation(s)

1. Calculate Velocity Head (a recurring term)

This term \( \frac{V^2}{2g} \) represents the fluid's kinetic energy per unit weight. It will be used again, so it's good to calculate it once:

\[ \begin{aligned} \frac{V^2}{2g} &= \frac{(5.80 \, \text{ft/s})^2}{2 \cdot 32.2 \, \text{ft/s}^2} \\ \frac{V^2}{2g} &= \frac{33.64}{64.4} \, \text{ft} \\ \frac{V^2}{2g} &\approx 0.522 \, \text{ft} \end{aligned} \]

This "velocity head" of 0.522 ft represents the fluid's velocity energy. We'll use this value in the next step.

2. Calculate Linear Head Loss

We apply the Darcy-Weisbach formula \( \Delta H_{\text{lin}} = f \cdot \frac{L}{D} \cdot \frac{V^2}{2g} \) by substituting all the values:

\[ \begin{aligned} \Delta H_{\text{lin}} &= f \cdot \left( \frac{L}{D} \right) \cdot \left( \frac{V^2}{2g} \right) \\ \Delta H_{\text{lin}} &= 0.0161 \cdot \left( \frac{656.2 \, \text{ft}}{0.328 \, \text{ft}} \right) \cdot (0.522 \, \text{ft}) \\ \Delta H_{\text{lin}} &\approx 0.0161 \cdot (2000.6) \cdot (0.522 \, \text{ft}) \\ \Delta H_{\text{lin}} &= 32.21 \cdot 0.522 \, \text{ft} \\ \Delta H_{\text{lin}} &\approx 16.81 \, \text{ft} \end{aligned} \]

By multiplying the friction factor (f), the length-to-diameter ratio (L/D), and the velocity head, we get a total linear head loss of 16.81 feet.

Diagram (After Calculation)
Visualization of Linear Head Loss
ABEnergy Grade Line (EGL)Major Head Loss: 16.81 ft
Reflections

A loss of 16.81 feet means the pressure in the fluid has dropped by an amount equivalent to the pressure exerted by a 16.81 ft column of water (approx. 7.3 psi). This is a non-negligible energy loss.

Caution

Verify that all quantities in the Darcy-Weisbach formula are in consistent units (feet, ft/s, ft/s²) before doing the numerical application.

Key Takeaways

The Darcy-Weisbach equation is central to hydraulics. Remember the quadratic influence of velocity (\(V^2\)) and the influence of the \(L/D\) ratio.

Did You Know?

Henry Darcy was a 19th-century French engineer who conducted pioneering experiments on water flow through sand beds in Dijon, laying the foundations for modern hydrogeology and hydraulics.

FAQ
Final Result
The major (linear) head loss is 16.81 feet.
Your Turn

If the pipe were 1312.4 ft long (double) instead of 656.2 ft, what would the new value of \(\Delta H_{\text{lin}}\) be?

Question 5: Calculate the minor (singular) head loss \(\Delta H_{\text{sing}}\)

Principle

Singular (or minor) head losses represent the "localized" energy loss caused by a disturbance in the flow. This disturbance is due to pipe fittings (elbows, valves, tees, reducers...) that force the fluid to change direction or velocity.

Mini-Lesson

Each fitting is characterized by a loss coefficient \(K\), which is a dimensionless number determined experimentally. The total head loss due to fittings is the sum of the individual losses, assuming the fittings are spaced far enough apart that their disturbances do not interfere with each other.

Pedagogical Note

In short circuits with many fittings (e.g., a mechanical room), minor losses can become dominant over major losses. Never neglect them without justification.

Standards

The \(K\) coefficients for standard fittings are tabulated in numerous fluid mechanics handbooks and professional standards (e.g., the Crane Technical Paper No. 410).

Formula(s)

Minor Head Loss Formula

\[ \Delta H_{\text{sing}} = \left( \sum K_i \right) \cdot \frac{V^2}{2g} \]
Assumptions

We assume the K-factors provided by manufacturers are correct and that the fittings are far enough apart that their disturbance effects do not overlap in a complex way.

Given Data
ParameterSymbolValueUnit
Loss Coefficient (Elbow)\(K_{\text{elbow}}\)0.9-
Loss Coefficient (Valve)\(K_{\text{valve}}\)0.2-
Velocity Head\(V^2/(2g)\)0.522ft
Tips

A minor loss can also be expressed as an "equivalent length" of straight pipe: \(L_{\text{eq}} = K \cdot D/f\). This allows you to combine all losses into a single linear loss calculation over a total fictitious length.

Diagram (Before Calculation)
Location of Minor Losses
K1K2K3
Calculation(s)

1. Sum of Loss Coefficients (K)

We add the K-factors for all fittings (2 elbows and 1 valve):

\[ \begin{aligned} \sum K_i &= (2 \times K_{\text{elbow}}) + K_{\text{valve}} \\ \sum K_i &= (2 \times 0.9) + 0.2 \\ \sum K_i &= 1.8 + 0.2 \\ \sum K_i &= 2.0 \end{aligned} \]

The sum of all K-factors for our fittings is 2.0 (dimensionless).

2. Calculate Minor Head Loss

We apply the formula \( \Delta H_{\text{sing}} = \left( \sum K_i \right) \cdot \frac{V^2}{2g} \). We reuse the velocity head \( \frac{V^2}{2g} \approx 0.522 \, \text{ft} \) calculated in step 4.

\[ \begin{aligned} \Delta H_{\text{sing}} &= \left( \sum K_i \right) \cdot \left( \frac{V^2}{2g} \right) \\ \Delta H_{\text{sing}} &= (2.0) \cdot (0.522 \, \text{ft}) \\ \Delta H_{\text{sing}} &= 1.04 \, \text{ft} \end{aligned} \]

The energy loss due to fittings is 1.04 feet, which is small compared to the linear losses.

Diagram (After Calculation)
Drop in Energy Grade Line at Fittings
K1K2Energy Grade Line
Reflections

The minor losses (1.04 ft) are much smaller than the major losses (16.81 ft) in this example because the pipe is long. This confirms that for long pipelines, linear friction losses are dominant.

Caution

Don't forget any fittings when counting the K-factors! A half-closed valve can have a K-factor of 5 or 10, radically changing the calculation.

Key Takeaways

The K-factor method is a simple and effective way to estimate localized losses. The loss is always proportional to the fluid's kinetic energy (\(V^2/2g\)).

Did You Know?

Golf balls have dimples for a reason related to head loss! These dimples create a thin turbulent boundary layer around the ball, which reduces "form drag" (a type of minor loss) and allows it to travel much farther than a smooth ball.

FAQ
Final Result
The minor (singular) head loss is 1.04 feet.
Your Turn

If we replaced the valve with a butterfly valve (K=1.5), what would the new \(\Delta H_{\text{sing}}\) be?

Question 6: Determine the total head loss \(\Delta H_{\text{tot}}\)

Principle

The total head loss is the sum of all energy losses experienced by the fluid along its path. It represents the total energy that the pump must supply to the fluid (per unit weight) just to maintain the flow, not counting any change in elevation or pressure between the inlet and outlet.

Mini-Lesson

In the generalized Bernoulli equation, which is the complete energy balance for a real fluid, \(\Delta H_{\text{tot}}\) appears as the loss term:
\(\frac{P_A}{\gamma} + \frac{V_A^2}{2g} + z_A + H_{\text{pump}} = \frac{P_B}{\gamma} + \frac{V_B^2}{2g} + z_B + \Delta H_{\text{tot}}\)

Pedagogical Note

This simple addition assumes that the disturbances from the fittings are spaced far enough apart not to interfere with each other. In practice, this is a very reliable approximation.

Formula(s)

Total Head Loss Formula

\[ \Delta H_{\text{tot}} = \Delta H_{\text{lin}} + \Delta H_{\text{sing}} \]
Assumptions

We assume that energy losses are additive, which is the standard assumption in hydraulics for pressurized flow.

Given Data
ParameterSymbolValueUnit
Major Head Loss\(\Delta H_{\text{lin}}\)16.81ft
Minor Head Loss\(\Delta H_{\text{sing}}\)1.04ft
Diagram (Before Calculation)
Summing the Head Losses
ΔHlinΔHsing+
Calculation(s)

We apply the formula \( \Delta H_{\text{tot}} = \Delta H_{\text{lin}} + \Delta H_{\text{sing}} \) by substituting the values from steps 4 and 5:

\[ \begin{aligned} \Delta H_{\text{tot}} &= \Delta H_{\text{lin}} + \Delta H_{\text{sing}} \\ \Delta H_{\text{tot}} &= 16.81 \, \text{ft} + 1.04 \, \text{ft} \\ \Delta H_{\text{tot}} &= 17.85 \, \text{ft} \end{aligned} \]

The total energy loss that the pump must overcome due to friction is 17.85 feet of water head.

Diagram (After Calculation)
Breakdown of Total Head Loss
Major (94%)16.81 ftMinor (6%)17.85 ft0 ft
Reflections

In this case (a long pipe), the major losses account for \(16.81 / 17.85 \approx 94\%\) of the total loss, while minor losses are only 6%. This justifies why minor losses can sometimes be neglected in very long pipelines, but major losses never can.

Caution

Ensure that \(\Delta H_{\text{lin}}\) and \(\Delta H_{\text{sing}}\) are in the same unit (feet) before adding them.

Key Takeaways

Total head loss is the sum of all major (friction over length) and minor (fittings) losses.

FAQ
Final Result
The total head loss for the circuit is 17.85 feet of fluid head.
Your Turn

Using \(\Delta H_{\text{lin}} = 16.81\) ft and the answer from Your Turn #5 (with the butterfly valve, \(\Delta H_{\text{sing}}\) = 1.72 ft), what would the new \(\Delta H_{\text{tot}}\) be?

Question 7: Calculate the power \(P\) dissipated (in horsepower)

Principle

The dissipated power (or "water horsepower") is the amount of energy lost by the fluid to friction, per unit of time. This is the power that the pump must add to the fluid just to overcome the head loss.

Mini-Lesson

This power is converted into heat. The "brake horsepower" (BHP) of the pump, which is the actual power required from the motor, will be even higher, as you must account for the pump's efficiency (e.g., \(P_{\text{brake}} = P_{\text{water}} / \eta_{\text{pump}}\)).

Pedagogical Note

The conversion factor 1 hp = 550 ft·lb/s is a fundamental constant in USCS fluid dynamics and thermodynamics. Memorizing it is essential.

Standards

The standard unit for pump power in the US is horsepower (hp).

Formula(s)

Water Horsepower Formula

\[ P \text{ (hp)} = \frac{\gamma \cdot Q \cdot \Delta H_{\text{tot}}}{550} \]
Assumptions

We assume the specific weight \(\gamma\) is constant throughout the circuit.

Given Data
ParameterSymbolValueUnit
Specific Weight\(\gamma\)62.4lb/ft³
Volume Flow RateQ0.490ft³/s
Total Head Loss\(\Delta H_{\text{tot}}\)17.85ft
Conversion Factor-550(ft·lb/s)/hp
Tips

You will often see the formula with GPM: \(P \text{ (hp)} = \frac{\text{GPM} \cdot \Delta H_{\text{tot}} \cdot (\text{Sp. Gr.})}{3960}\). This is a derived formula that includes all the conversion factors (GPM to ft³/s, and \(\gamma\)). Let's check: \((220 \cdot 17.85 \cdot 1.0) / 3960 \approx 0.992 \text{ hp}\). It works! Our fundamental formula is more precise.

Diagram (Before Calculation)
Concept of Dissipated Power
ABΔHtot (Energy Loss)Q (Flow Rate)
Calculation(s)

First, we calculate the power in ft·lb/s using the formula \( P = \gamma \cdot Q \cdot \Delta H_{\text{tot}} \). We must use \(Q\) in ft³/s.

\[ \begin{aligned} P \text{ (ft}\cdot\text{lb/s)} &= \gamma \cdot Q \cdot \Delta H_{\text{tot}} \\ P &= (62.4 \, \frac{\text{lb}}{\text{ft}^3}) \cdot (0.490 \, \frac{\text{ft}^3}{\text{s}}) \cdot (17.85 \, \text{ft}) \\ P &\approx 546.0 \, \text{ft}\cdot\text{lb/s} \end{aligned} \]

Next, we convert this value to horsepower by dividing by 550.

\[ \begin{aligned} P \text{ (hp)} &= \frac{P \text{ (ft}\cdot\text{lb/s)}}{550} \\ P \text{ (hp)} &= \frac{546.0}{550} \\ P \text{ (hp)} &\approx 0.993 \, \text{hp} \end{aligned} \]

The product of these values gives us the dissipated power, which is approximately 0.993 horsepower.

Diagram (After Calculation)
Power Balance
CircuitP (pump)P (useful) P (dissipated) = 0.99 hp
Reflections

A power of 0.993 hp (or 741 W) is continuously converted into heat. The pump must supply at least this much "water horsepower". The actual "brake horsepower" required by the pump motor will be higher, e.g., if the pump is 75% efficient, the motor must provide \(0.993 / 0.75 \approx 1.32 \text{ hp}\).

Caution

The most common error is mismatching units in the power formula. Do NOT use GPM directly in the fundamental power equation. You must convert to ft³/s first, or use the "shortcut" formula (like the one in "Tips") which has the conversions built-in.

Key Takeaways

The water horsepower is the product of the fluid's specific weight (\(\gamma\)), the flow rate in ft³/s (\(Q\)), and the total head loss (\(\Delta H_{\text{tot}}\)), divided by 550.

Did You Know?

In large oil pipelines spanning thousands of miles, head losses are so significant that powerful pumping stations (often thousands of horsepower) must be installed every 50 to 100 miles to "re-boost" the pressure.

FAQ
Final Result
The power dissipated by head loss is approximately 0.993 horsepower.
Your Turn

If the total head loss were 30 ft, what would the dissipated power be (in hp)?


Interactive Tool: Head Loss Simulator

Use the sliders to see how flow rate and pipe diameter influence the total head loss and dissipated power. Other parameters (length, roughness, etc.) remain fixed.

Input Parameters
220 GPM
3.94 in
Key Results
Total Head Loss (\(\Delta H_{\text{tot}}\)) - ft
Dissipated Power (P) - hp

Final Quiz: Test Your Knowledge

1. What does the Reynolds number primarily represent?

2. Major (linear) head loss is directly proportional to:

3. What causes a minor (singular) head loss?

4. If you increase a pipe's roughness, the friction factor \(f\) for turbulent flow will:

5. In the US Customary System, a common unit for pump power is:


Glossary

Head Loss
Represents the energy loss (expressed as a height of fluid, in feet or meters) of a moving fluid due to friction.
Reynolds Number (Re)
A dimensionless number used in fluid mechanics to characterize a flow regime. It quantifies the ratio of inertial forces to viscous forces.
Friction Factor (f)
A dimensionless coefficient used in the calculation of linear head loss, which depends on pipe roughness and the Reynolds number.
Roughness (\(\varepsilon\))
A measure of the surface imperfections inside a pipe, which influences fluid friction.
Specific Weight (\(\gamma\))
The weight of a fluid per unit volume (e.g., lb/ft³). For water, this is approximately 62.4 lb/ft³.
Exercise: Power Dissipated by Head Loss
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