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Module "aerodynamics/nuFromMach"

Index

Functions

Functions

nuFromMach

  • nuFromMach(mach: number, y?: number): number

  • Calculate the value of the Prandtl-Meyer angle (ν) based on a given Mach number and ratio of specific heats

    Parameters

    • mach: number

      Mach number for which you want to obtain the value of nu

    • Default value y: number = 1.4

      Ratio of specific heats of the gas used

    Returns number

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