Prandtl-Meyer angle after the deflection at wedge Calculator

The Prandtl-Meyer angle () after a deflection at a wedge refers to the change in the Prandtl-Meyer angle due to the deflection of a supersonic flow around a wedge-shaped body or surface. The Prandtl-Meyer angle is a critical concept in supersonic aerodynamics that characterizes the angular deviation of the flow direction from a reference direction. 
  • Prandtl-Meyer angle after the deflection (v2) in rad
  • Prandtl-Meyer angle before the deflection (v1) in rad
  • Wedge angle (α) in rad

Leave a Comment

Your email address will not be published.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

Scroll to Top