The Mechanical Engineering Handbook



Advance Ratio

Advance Ratio Equation



$$ J = \frac{v_0}{nD} $$ where:

J   =   Advance Ratio (Dimensionless)

v_0   =   Freestream Velocity   (m/s)

n   =   Propeller rotational speed   (rev/s)

D   =   Diameter of the propeller   (m)


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Equation Assumptions



  • The system is in steady state.
  • Fluid is incompressible.
  • The flow is at the propeller disk is uniform.
  • The fluid behaves as an ideal gas.
  • There are no propeller interaction effects.