Area Ratio of Nozzle in Rocket Propulsion Formulas

The Area Ratio of Nozzle refers to the ratio of the cross-sectional area of the exit (throat) of the nozzle to the cross-sectional area of the exit (exit plane) of the nozzle. And is denoted by ∈.

Formulas to find Area Ratio of Nozzle in Rocket Propulsion

fxArea Ratio of NozzlesGo

List of variables in Rocket Propulsion formulas

fx Mach at Exit Go

fx Specific Heat Ratio Go

FAQ

What is the Area Ratio of Nozzle?

The Area Ratio of Nozzle refers to the ratio of the cross-sectional area of the exit (throat) of the nozzle to the cross-sectional area of the exit (exit plane) of the nozzle.

Can the Area Ratio of Nozzle be negative?

{YesorNo}, the Area Ratio of Nozzle, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

Let Others Know

✖

Facebook

Twitter

Copied!