Prandtl–Meyer expansion fan - last Mach line angle

Description

A supersonic expansion fan, technically known as Prandtl–Meyer expansion fan, is a centred expansion process that occurs when a supersonic flow turns around a convex corner. The fan consists of an infinite number of Mach waves, diverging from a sharp corner. When a flow turns around a smooth and circular corner, these waves can be extended backwards to meet at a point.

Each wave in the expansion fan turns the flow gradually (in small steps). It is physically impossible for the flow to turn through a single “shock” wave because this would violate the second law of thermodynamics.

The expansion fan consists of infinite number of expansion waves or Mach lines.The last Mach line is at an angle calculated by the shown formula

Related formulas

Variables

μ2angle of last Mach line with respect to final flow direction (radian)
M2last line Mach number (dimensionless)