MECHANICAL ENGINEERING TOOLS, CALCULATORS, SOFTWARE
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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 Speed of Sound at the Exit - SuperSonic Nozzle
PHP Calculator v1
Heat capacity ratio
:
It is 1.4 for air at 20°C.
See more
Te
(The Temperature at the Exit):
K (Kelvin)
R
(Gas Constant per unit mass):
It is 287 for air at standart conditions. (J / kg. K)
Coded by Umut Aksoy
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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