Module "aerospace/expansionRatio"

expansionRatio

• expansionRatio(p: number, p_c: number, y?: number): number

• From: https://link.springer.com/chapter/10.1007/978-3-319-74373-8_4

  Parameters

  • p: number

    Pressure [Pa]

  • p_c: number

    Pressure in the combustion chamber [Pa]

  • Default value y: number = 1.4

    Ratio of specific heats [-]

  Returns number