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fluids-packagePipe flow, pump sizing, friction factor, and compressible flow calculations
Independent GitHub snapshot · Automated classification · Original documentation governs
name: fluids-package description: "Pipe flow, pump sizing, friction factor, and compressible flow calculations" category: packages domain: fluids complexity: intermediate dependencies:
The fluids library is a comprehensive Python package for mechanical and chemical engineers working with fluid flow problems. It provides validated correlations and functions for:
The library implements over 100 correlations from the literature with extensive validation against published test cases.
pip install fluids
For full functionality including optimization routines:
pip install fluids[complete]
Core utilities and dimensional analysis functions.
Friction factor calculations for pipe flow including:
Pump performance calculations:
Compressible flow calculations:
Pressure drop through valves, fittings, and pipe components.
The Reynolds number (Re) determines flow regime and is fundamental to all pipe flow calculations.
from fluids.core import Reynolds
# For pipe flow: Re = ρVD/μ
Re = Reynolds(V=2.5, D=0.05, rho=1000, mu=0.001)
# Result: 125000 (turbulent flow)
# Interpretation:
# Re < 2300: Laminar flow
# 2300 < Re < 4000: Transition
# Re > 4000: Turbulent flow
The friction factor (f) is used in the Darcy-Weisbach equation: ΔP = f(L/D)(ρV²/2)
from fluids.friction import friction_factor
# Colebrook-White correlation (implicit, most accurate)
f = friction_factor(Re=125000, eD=0.0001) # eD = roughness/diameter
# Result: ~0.0178
# Moody correlation (explicit approximation)
from fluids.friction import friction_factor_Moody
f_moody = friction_factor_Moody(Re=125000, eD=0.0001)
# For laminar flow (Re < 2300):
f_laminar = friction_factor(Re=1500, eD=0.0001)
# Result: 0.0427 (f = 64/Re)
Calculate pressure drop and head loss in piping systems.
from fluids.friction import friction_factor, head_from_P
from fluids.core import Reynolds
# Given: Water flow through steel pipe
D = 0.1 # m, pipe diameter
L = 100 # m, pipe length
V = 2.0 # m/s, velocity
rho = 1000 # kg/m³, density
mu = 0.001 # Pa·s, viscosity
epsilon = 0.000045 # m, roughness (steel)
# Step 1: Calculate Reynolds number
Re = Reynolds(V=V, D=D, rho=rho, mu=mu)
# Step 2: Calculate friction factor
eD = epsilon / D
f = friction_factor(Re=Re, eD=eD)
# Step 3: Calculate pressure drop
# Darcy-Weisbach: ΔP = f(L/D)(ρV²/2)
dP = f * (L/D) * (rho * V**2 / 2)
# Step 4: Convert to head loss
h_loss = head_from_P(dP, rho) # meters of fluid
print(f"Reynolds: {Re:.0f}")
print(f"Friction factor: {f:.5f}")
print(f"Pressure drop: {dP:.0f} Pa")
print(f"Head loss: {h_loss:.2f} m")
Relate pump performance at different speeds and impeller diameters.
from fluids.pump import affinity_law_volume, affinity_law_head, affinity_law_power
# Original pump operating point
Q1 = 100 # m³/h, flow rate
H1 = 50 # m, head
P1 = 20 # kW, power
N1 = 1450 # rpm, speed
D1 = 0.3 # m, impeller diameter
# New speed
N2 = 1750 # rpm
# Affinity laws (constant impeller diameter):
# Q2/Q1 = N2/N1
# H2/H1 = (N2/N1)²
# P2/P1 = (N2/N1)³
Q2 = affinity_law_volume(Q1, N1, N2)
H2 = affinity_law_head(H1, N1, N2)
P2 = affinity_law_power(P1, N1, N2)
print(f"New flow: {Q2:.1f} m³/h")
print(f"New head: {H2:.1f} m")
print(f"New power: {P2:.1f} kW")
Specific speed (Ns) characterizes pump type and efficiency.
from fluids.pump import specific_speed
# Pump operating conditions
Q = 0.05 # m³/s, flow rate
H = 40 # m, head
N = 1450 # rpm, rotational speed
# Calculate specific speed (dimensionless)
Ns = specific_speed(Q, H, N)
# Interpretation:
# Ns < 0.5: Centrifugal (radial flow)
# 0.5 < Ns < 1.0: Francis (mixed flow)
# 1.0 < Ns < 4.0: Propeller (axial flow)
print(f"Specific speed: {Ns:.2f}")
if Ns < 0.5:
pump_type = "Centrifugal (radial flow)"
elif Ns < 1.0:
pump_type = "Francis (mixed flow)"
else:
pump_type = "Propeller (axial flow)"
print(f"Recommended pump type: {pump_type}")
For gas flow in pipes and nozzles.
from fluids.compressible import Mach
# Calculate Mach number from velocity
V = 200 # m/s, velocity
c = 340 # m/s, speed of sound in air at 15°C
Ma = Mach(V, c)
# Result: 0.588
# Flow classification:
# Ma < 0.3: Incompressible
# 0.3 < Ma < 0.8: Subsonic
# 0.8 < Ma < 1.2: Transonic
# Ma > 1.2: Supersonic
Determine if flow is choked in a nozzle or orifice.
from fluids.compressible import P_critical_flow
# Gas properties
P_upstream = 500000 # Pa, upstream pressure
k = 1.4 # heat capacity ratio (air)
# Critical pressure for choked flow
P_crit = P_critical_flow(P=P_upstream, k=k)
# Result: ~264,000 Pa
# If downstream pressure < P_crit, flow is choked
P_downstream = 200000 # Pa
if P_downstream < P_crit:
print("Flow is choked - mass flow is at maximum")
print(f"Critical pressure: {P_crit:.0f} Pa")
else:
print("Flow is not choked")
import numpy as np
from fluids.friction import friction_factor
from fluids.core import Reynolds
import matplotlib.pyplot as plt
def system_curve(Q_range, static_head, pipe_specs):
"""
Calculate system head curve for a piping system.
Parameters:
-----------
Q_range : array, flow rates (m³/s)
static_head : float, static lift (m)
pipe_specs : dict with keys:
- L: pipe length (m)
- D: pipe diameter (m)
- epsilon: roughness (m)
- rho: fluid density (kg/m³)
- mu: fluid viscosity (Pa·s)
Returns:
--------
H_system : array, required head at each flow rate (m)
"""
L = pipe_specs['L']
D = pipe_specs['D']
rho = pipe_specs['rho']
mu = pipe_specs['mu']
epsilon = pipe_specs['epsilon']
# Calculate cross-sectional area
A = np.pi * D**2 / 4
H_system = np.zeros_like(Q_range)
for i, Q in enumerate(Q_range):
if Q == 0:
H_system[i] = static_head
continue
# Calculate velocity
V = Q / A
# Reynolds number
Re = Reynolds(V=V, D=D, rho=rho, mu=mu)
# Friction factor
eD = epsilon / D
f = friction_factor(Re=Re, eD=eD)
# Friction head loss (Darcy-Weisbach)
h_friction = f * (L/D) * (V**2 / (2*9.81))
# Total system head
H_system[i] = static_head + h_friction
return H_system
# Define system
pipe_specs = {
'L': 200, # m
'D': 0.15, # m
'epsilon': 0.000045, # m (steel)
'rho': 1000, # kg/m³
'mu': 0.001 # Pa·s
}
static_head = 30 # m
# Generate system curve
Q_range = np.linspace(0, 0.1, 50) # m³/s
H_system = system_curve(Q_range, static_head, pipe_specs)
# Example pump curve (quadratic fit)
# H = H0 - A*Q - B*Q²
H0 = 80 # m, shutoff head
A = 200 # head loss coefficient
B = 3000 # quadratic coefficient
H_pump = H0 - A*Q_range - B*Q_range**2
# Find operating point (intersection)
idx = np.argmin(np.abs(H_pump - H_system))
Q_op = Q_range[idx]
H_op = H_system[idx]
print(f"Operating Point:")
print(f" Flow rate: {Q_op*3600:.1f} m³/h ({Q_op:.4f} m³/s)")
print(f" Head: {H_op:.1f} m")
# Verification: At Q=0.05 m³/s
# V = Q/A = 0.05/(π*0.15²/4) = 2.83 m/s
# Re = 1000*2.83*0.15/0.001 = 424,500 (turbulent)
# f ≈ 0.0175 (from Moody chart)
# h_f = 0.0175*(200/0.15)*(2.83²/(2*9.81)) = 9.5 m
# H_total = 30 + 9.5 = 39.5 m ✓
from fluids.pump import affinity_law_volume, affinity_law_head
def parallel_pumps(Q_total, n_pumps, single_pump_curve):
"""
Calculate operating point for parallel pump configuration.
For pumps in parallel:
- Flow rates add: Q_total = n * Q_single
- Head remains the same: H_total = H_single
"""
# Single pump flow rate
Q_single = Q_total / n_pumps
# Head from single pump curve
H = single_pump_curve(Q_single)
return Q_single, H
# Single pump curve: H = 60 - 500*Q² (simplified)
def pump_curve(Q):
return 60 - 500*Q**2
# System requires 150 m³/h at 40 m head
Q_required = 150/3600 # m³/s
n_pumps = 2
Q_single, H_operating = parallel_pumps(Q_required, n_pumps, pump_curve)
print(f"Parallel Pump Configuration ({n_pumps} pumps):")
print(f" Total flow: {Q_required*3600:.1f} m³/h")
print(f" Flow per pump: {Q_single*3600:.1f} m³/h")
print(f" Operating head: {H_operating:.1f} m")
# Verification:
# Each pump delivers 75 m³/h (0.0208 m³/s)
# H = 60 - 500*(0.0208)² = 60 - 0.22 = 59.8 m ✓
from fluids.friction import friction_factor, friction_factor_laminar
# Test Case 1: Laminar Flow (Poiseuille)
# Analytical solution: f = 64/Re
Re_laminar = 1000
f_calculated = friction_factor(Re=Re_laminar, eD=0)
f_analytical = 64/Re_laminar
print("Test 1: Laminar Flow")
print(f" Re = {Re_laminar}")
print(f" f (calculated) = {f_calculated:.6f}")
print(f" f (analytical) = {f_analytical:.6f}")
print(f" Error = {abs(f_calculated - f_analytical):.9f}")
assert abs(f_calculated - f_analytical) < 1e-9, "Laminar flow test failed"
print(" ✓ PASSED\n")
# Test Case 2: Turbulent Flow - Smooth Pipe
# From Moody diagram: Re=1e5, smooth pipe → f ≈ 0.0183
Re_turbulent = 1e5
f_smooth = friction_factor(Re=Re_turbulent, eD=0)
print("Test 2: Turbulent Flow (Smooth Pipe)")
print(f" Re = {Re_turbulent:.0f}")
print(f" f (calculated) = {f_smooth:.6f}")
print(f" f (Moody chart) ≈ 0.0183")
print(f" Error = {abs(f_smooth - 0.0183):.6f}")
assert abs(f_smooth - 0.0183) < 0.0005, "Smooth pipe test failed"
print(" ✓ PASSED\n")
# Test Case 3: Turbulent Flow - Rough Pipe
# Commercial steel: ε/D = 0.0002, Re = 1e6 → f ≈ 0.0144
Re_rough = 1e6
eD_rough = 0.0002
f_rough = friction_factor(Re=Re_rough, eD=eD_rough)
print("Test 3: Turbulent Flow (Rough Pipe)")
print(f" Re = {Re_rough:.0f}")
print(f" ε/D = {eD_rough}")
print(f" f (calculated) = {f_rough:.6f}")
print(f" f (Moody chart) ≈ 0.0144")
print(f" Error = {abs(f_rough - 0.0144):.6f}")
assert abs(f_rough - 0.0144) < 0.0005, "Rough pipe test failed"
print(" ✓ PASSED\n")
# Test Case 4: From Crane TP-410 (Standard reference)
# Example 4-9: Water in 6-inch Schedule 40 pipe
D = 0.1541 # m (6-inch Schedule 40 ID)
V = 3.05 # m/s
rho = 998 # kg/m³
mu = 0.001 # Pa·s
epsilon = 0.000045 # m (steel)
Re_crane = Reynolds(V=V, D=D, rho=rho, mu=mu)
eD_crane = epsilon/D
f_crane = friction_factor(Re=Re_crane, eD=eD_crane)
# Crane TP-410 gives f ≈ 0.0172
print("Test 4: Crane TP-410 Example 4-9")
print(f" Re = {Re_crane:.0f}")
print(f" ε/D = {eD_crane:.6f}")
print(f" f (calculated) = {f_crane:.6f}")
print(f" f (Crane TP-410) ≈ 0.0172")
print(f" Error = {abs(f_crane - 0.0172):.6f}")
assert abs(f_crane - 0.0172) < 0.0003, "Crane TP-410 test failed"
print(" ✓ PASSED\n")
print("All friction factor tests passed! ✓")
from fluids.compressible import isothermal_gas
# Gas pipeline calculation
# Problem: Natural gas (methane) pipeline
P1 = 5e6 # Pa, inlet pressure
T = 288.15 # K, temperature (15°C)
L = 50000 # m, pipeline length (50 km)
D = 0.5 # m, diameter
m = 10 # kg/s, mass flow rate
MW = 16.04 # g/mol, molecular weight (CH4)
k = 1.31 # heat capacity ratio
# Calculate outlet pressure using isothermal flow
# This accounts for friction and compressibility
from fluids.compressible import isothermal_gas
P2 = isothermal_gas(rho=None, P1=P1, P2=None, L=L, D=D, m=m,
T=T, Z=1, fd=0.012) # Assuming f=0.012
print("Gas Pipeline Calculation:")
print(f" Inlet pressure: {P1/1e6:.2f} MPa")
print(f" Outlet pressure: {P2/1e6:.2f} MPa")
print(f" Pressure drop: {(P1-P2)/1e6:.2f} MPa")
print(f" Length: {L/1000:.0f} km")
print(f" Mass flow: {m:.1f} kg/s")
| Material | Roughness ε (m) |
|---|---|
| Drawn tubing | 0.0000015 |
| Commercial steel | 0.000045 |
| Galvanized iron | 0.00015 |
| Cast iron | 0.00026 |
| Concrete | 0.0003 to 0.003 |
| Riveted steel | 0.0009 to 0.009 |