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Converging-Diverging Nozzle
Description
Precision:
Ratio of specific heats
γ
Ideal gas constant (J kg
-1
K
-1
)
R
Total pressure (Pa)
p
0
Total temperature (K)
T
0
Throat area (m
2
)
A
throat
Exit area (m
2
)
A
exit
Maximum back pressure for sonic throat (Pa)
p
sub
Back pressure for shock at exit (Pa)
p
shock
Design back pressure (Pa)
p
design
Design exit Mach number
Ma
design
Maximum mass flow rate (kg s
-1
)
mdot
max