Module "aerodynamics/normalShockProperties"

normalShockProperties

• normalShockProperties(mach: number, y?: number): number[]

• Calculate the normal shock properties for a given Mach number and ratio of specific heats.

  Parameters

  • mach: number

    Mach number for which you want to obtain the normal shock properties

  • Default value y: number = 1.4

    Ratio of specific heats of the gas used

  Returns number[]