Dynamic Pressure (q = ½ρv²)

q=12ρv2q = \tfrac{1}{2} \rho v^{2}

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Dynamic pressure is 12mv2\tfrac{1}{2}mv^2 written per unit volume, and it is what a moving fluid can push with when brought to rest. An aircraft's pitot tube measures exactly this — the difference between ram pressure facing the flow and static pressure beside it — and converts it back to airspeed via v=2q/ρv = \sqrt{2q/\rho}. A 30 m/s wind (about 108 km/h) carries q=12×1.225×302551 Paq = \tfrac{1}{2} \times 1.225 \times 30^2 \approx 551\ \text{Pa}, over half a kilonewton on every square meter of a billboard.

Dynamic Pressure (q = ½ρv²)
q=12ρv2q = \tfrac{1}{2} \rho v^{2}
Where
  • qq= Dynamic pressure
  • ρ\rho= Fluid density
  • vv= Flow velocity
Missing one of these? Work it out first, then come back