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Bernoulli and the Venturi Effect

Steady incompressible flow through a pipe with a constriction. Mass conservation forces Q=A(x)v(x)=constQ = A(x)\,v(x) = \text{const}, so the fluid speeds up where the pipe narrows; Bernoulli's theorem p+12ρv2=constp + \tfrac12\rho v^2 = \text{const} (horizontal pipe) then forces the static pressure down exactly where the speed is up. The piezometer columns make this visible: they are tall in the wide sections and dip at the throat, the Venturi effect. Tracer particles accelerate through the throat (v1/Av \propto 1/A). The same principle is the cartoon airfoil: faster flow over the curved top means lower pressure and net upward lift. The headline readouts are the two invariants, the relative spread of the Bernoulli constant and of the flux AvA v along the pipe, both held below 10310^{-3} because the model is the exact algebra, not a simulation.

Figure 1. Steady incompressible flow in a variable-area pipe: continuity (AvA v constant) accelerates the flow at the throat and Bernoulli (p+12ρv2p + \tfrac12\rho v^2 constant) drops the static pressure there, shown by the dipping piezometer columns; the inset is the same principle producing airfoil lift. Method: closed-form continuity and Bernoulli (no simulation), Canvas2D; the live readouts are the relative spread of the two conserved quantities.
throat ratio0.40
flow rate Q0.70
density rho1.2

WHAT TO TRY

  • Vary each control and watch the rail readouts respond.
  • Compare the diagnostic plot against the live scene.