Options
All
  • Public
  • Public/Protected
  • All
Menu

Module "aerodynamics/machFromNu"

Index

Functions

Functions

machFromNu

  • machFromNu(nu: number): number
  • Compute the value of the Mach number based on a given Prandtl-Meyer angle. The accurarcy of this Hall approximation is quite good with the maximum error being much less than one-tenth of one percent. The source for this approximation can be found here.

    Parameters

    • nu: number

      Value of nu for which you would like to calculate the Mach number

    Returns number

Generated using TypeDoc