Calculate Mass Flow at the Exit (Method 2) - SuperSonic Nozzle

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Nozzle Combustion Chamber

Calculate Combustion Chamber Gas Density

Calculate Combustion Chamber Pressure

Nozzle Throat

Calculate Throat Gas Density

Calculate Throat Mach Number

Calculate Throat Temperature

Calculate Throat Velocity

Calculate Throat Pressure

Calculate Throat Mass Flow

Calculate the Speed of Sound at Throat

Calculate Throat Area

Nozzle Exit

Calculate Exit Gas Density

Calculate Exit Mach Number

Calculate Exit Temperature

Calculate Exit Velocity (1)

Calculate Exit Velocity (2)

Calculate Exit Pressure

Calculate Exit Mass Flow (1)

Calculate Exit Mass Flow (2)

Calculate the Speed of Sound at Exit

Calculate Exit Area

Other Parameters

Calculate Gas Constant per Unit Mass

Calculate Pressure Coefficient

Calculate Thrust

Calculate Mass Flow at the Exit (Method 2) - SuperSonic Nozzle

PHP Calculator v1


Thrust (At the Exit)		N (Newton)
Ve (The Velocity at the Exit):		m/s


Coded by Umut Aksoy

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Parameters

P(c): Combustion Chamber Pressure
T(c): Combustion Chamber Temperature
T(t): Throat Temperature
P(t): Throat Pressure
V(t): Velocity at the Throat
A(t): Throat Area
T(e): Exit Temperature
P(e): Exit Pressure
V(e): Velocity at the Exit
A(e): Exit Area

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