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Propulsion
Nozzle Exit Area in Jet Propulsion Formulas
Nozzle Exit Area refers to the cross-sectional area at the exit of a nozzle. And is denoted by A
e
. Nozzle Exit Area is usually measured using the Square Meter for Area. Note that the value of Nozzle Exit Area is always positive.
Formulas to find Nozzle Exit Area in Jet Propulsion
f
x
Nozzle Exit Area in Turbojet
Go
Jet Propulsion formulas that make use of Nozzle Exit Area
f
x
Turbojet Gross Thrust
Go
f
x
Exhaust Velocity given Gross Thrust in Turbojet
Go
f
x
Net Thrust Produced by Turbojet
Go
f
x
Exhaust Velocity given Thrust in Turbojet
Go
f
x
Flight Speed given Thrust in Turbojet
Go
f
x
Mass Flow Rate of Turbojet given Gross Thrust
Go
f
x
Mass Flow Rate in Turbojet given Thrust
Go
List of variables in Jet Propulsion formulas
f
x
Net Thrust of Turbojet
Go
f
x
Mass Flow Rate Turbojet
Go
f
x
Fuel Air Ratio
Go
f
x
Exit Velocity
Go
f
x
Flight Speed
Go
f
x
Nozzle Exit Pressure
Go
f
x
Ambient Pressure
Go
FAQ
What is the Nozzle Exit Area?
Nozzle Exit Area refers to the cross-sectional area at the exit of a nozzle. Nozzle Exit Area is usually measured using the Square Meter for Area. Note that the value of Nozzle Exit Area is always positive.
Can the Nozzle Exit Area be negative?
No, the Nozzle Exit Area, measured in Area cannot be negative.
What unit is used to measure Nozzle Exit Area?
Nozzle Exit Area is usually measured using the Square Meter[m²] for Area. Square Kilometer[m²], Square Centimeter[m²], Square Millimeter[m²] are the few other units in which Nozzle Exit Area can be measured.
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