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Pitot Tubes

Reference data and engineering information about pitot tubes for fluid mechanics applications.

pitottubes

Overview

Engineering reference data for Pitot Tubes in fluid mechanics.

Key Formulas

Reynolds Number

Re=ρvDμRe = \frac{\rho v D}{\mu}

Ratio of inertial to viscous forces — determines flow regime.

Bernoulli's Equation

P+12ρv2+ρgh=constP + \frac{1}{2}\rho v^2 + \rho g h = \text{const}

Conservation of energy for steady, inviscid, incompressible flow.

Continuity Equation

A1v1=A2v2A_1 v_1 = A_2 v_2

Conservation of mass for incompressible flow.

Darcy-Weisbach

ΔP=fLDρv22\Delta P = f \frac{L}{D} \frac{\rho v^2}{2}

Pressure drop due to friction in a pipe.

Variables

SymbolDescriptionUnit
ReReReynolds number
ρ\rhoFluid densitykg/m³
vvFlow velocitym/s
DDCharacteristic dimensionm
μ\muDynamic viscosityPa·s
PPPressurePa
ffDarcy friction factor

Key Formulas

The following equations are fundamental to pitot tube operation and flow measurement:

p+12ρv2+ρgh=constant along a streamline(1)p + \frac{1}{2} \rho v^2 + \rho g h = \text{constant along a streamline} \quad (1) p1+12ρv12=p2(3)p_1 + \frac{1}{2} \rho v_1^2 = p_2 \quad (3) v1=2(p2p1)ρ=2Δpρ(4)v_1 = \sqrt{\frac{2 (p_2 - p_1)}{\rho}} = \sqrt{\frac{2 \Delta p}{\rho}} \quad (4) v1=c2gΔh(5)v_1 = c \sqrt{2 g \Delta h} \quad (5) va=vnn=2ghnn(6)v_a = \frac{\sum v_n}{n} = \sqrt{\frac{2 g \sum h_n}{n}} \quad (6) q=vaA(7)q = v_a A \quad (7)

Pressure Definitions

Each term in the Bernoulli equation represents a specific type of pressure:

  • Static Pressure (pp): The pressure relative to the moving fluid, measurable through a flat opening parallel to the flow.
  • Dynamic Pressure (12ρv2\frac{1}{2} \rho v^2): The pressure component due to the fluid's kinetic energy.
  • Hydrostatic Pressure (ρgh\rho g h or γh\gamma h): The pressure component due to the fluid's elevation, where γ=ρg\gamma = \rho g is the specific weight.

Measurement & Application

The pitot tube measures the difference between total (stagnation) pressure at the tip and static pressure from the side ports. This pressure difference (Δp\Delta p or Δh\Delta h) is used with equations (4) or (5) to calculate the point velocity in the free stream.

For flow rate determination in a conduit, the point velocity-area method is used. Point velocities are measured across a traverse, and the average velocity (vav_a) is calculated using equation (6). The volume flow (qq) is then found from equation (7).

Practical Guidance:

  • For round ducts larger than 10 inches (254 mm), a 10-point traverse is recommended at specific radial positions.
  • For smaller ducts, the average velocity can be estimated as 81% of the centerline velocity.
  • Pitot tubes are not suited for low-velocity flows due to the small dynamic pressure differential, which leads to inaccurate readings.

References