Pitot Tube Calculator
Flow speed from dynamic pressure: v = √(2ΔP/ρ)
Parameters
Controls
Calculated Values
Examples
Air ΔP=500 Pa
ρ=1.2 kg/m³.
Water probe
ΔP=10 kPa.
Visualization
Pitot Tube — Velocity from Stagnation Pressure
A Pitot tube (Henri Pitot, 1732; improved by Henri Darcy) measures fluid velocity by sensing stagnation (total) pressure where the flow is brought to rest at the probe tip. From Bernoulli along a streamline: P₀ = P + ½ρv², where P₀ is stagnation pressure, P is static pressure, and v is approach velocity.
Dynamic pressure q = ½ρv² = P₀ − P = ΔP. Solving gives v = √(2ΔP/ρ). Units check: √(Pa/(kg/m³)) = √(m²/s²) = m/s. For air at ρ = 1.2 kg/m³ and ΔP = 500 Pa, v ≈ √(1000/1.2) ≈ 29 m/s (~105 km/h).
A Pitot-static probe has two ports: forward-facing (stagnation) and side ports (static pressure in undisturbed flow). Aircraft pitot tubes feed airspeed indicators; calibration accounts for altitude (density) and compressibility at high Mach number.
The probe must point directly into the flow — misalignment causes underestimation. Blockage, ice formation (aviation hazard), and turbulence can cause errors. In pipes, velocity varies across the section — traverse measurements at several radii are needed for average flow.
Relation to other formulas: Torricelli v = √(2gh) is the same with ΔP = ρgh. Venturi measures volume flow from ΔP; Pitot measures point velocity. Dynamic pressure appears in drag formulas (pressure drag scales with ρv²).
Compressible corrections at high subsonic/supersonic speeds use isentropic relations. For incompressible water or low-speed air, v = √(2ΔP/ρ) is standard in hydraulics labs and wind tunnels.
Key Concepts
- P₀ = P + ½ρv² (Bernoulli stagnation)
- v = √(2ΔP/ρ); q = ½ρv²
- Pitot-static: stagnation vs static ports
- ΔP = dynamic pressure (Pa)
- Must align probe with flow vector
- Local v, not average — traverse for Q
Real-World Applications
- Aircraft airspeed and altitude instruments
- Wind tunnel velocity calibration
- River, pipe, and duct flow profiling
- Formula 1 and aerospace aerodynamic testing
- Class 12 Bernoulli and Pitot demonstrations
- Industrial anemometry and HVAC traverse
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Physics Equations
Step-by-Step Solution
See how the main results are calculated.
Step 1: Stagnation Pressure
Equation:
Explanation:
Flow stops at stagnation point; KE → pressure.
Step 2: Pitot Relation
Equation:
Explanation:
ΔP = P₀ − P (dynamic pressure).
Step 3: Substitute
Calculation:
Result:
Step 4: Check Units
ΔP in Pa, ρ in kg/m³ → v in m/s.
Explanation:
√(Pa/(kg/m³)) = √(m²/s²) = m/s.
Step 5: Applications
Aircraft airspeed, pipe velocity.
Explanation:
Correct for compressibility at high Mach.
Step 6: Bernoulli Link
Same as Torricelli with ΔP = ρgh.
Explanation:
Pitot measures local flow speed.
Frequently Asked Questions (FAQ)
Pitot vs Venturi?
Pitot: point velocity from ΔP; Venturi: integrated Q in pipe.
Compressibility?
High-speed air needs isentropic corrections.
Water hammer?
Different phenomenon — pressure transients.
Two holes?
Pitot-static: stagnation + static ports.
Turbulent profile?
Pitot gives local v; traverse for average.
Practice MCQs
- Stagnation pressure is:
- v from Pitot scales as:
- Pitot measures:
- ΔP = 0 means:
- Bernoulli assumes:
- Pitot hole misaligned:
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