Critical pressure coefficient with respect to freestream Mach number Calculator

The critical pressure coefficient () is a specific value of the pressure coefficient () at a particular location on an airfoil or aerodynamic surface where the flow reaches a critical condition. This condition is typically associated with the onset of flow separation or the point at which the flow detaches from the surface. 

  • Specific heat ratio (γ) 
  • Freestream Mach number (M∞) 
  • Critical pressure coefficient (Cp,cr)

Leave a Comment

Your email address will not be published. Required fields are marked *

Scroll to Top