What is the thrust of an engine if the inlet and exhaust mass flow rate are 150 kg/s and 190 kg/s respectively with the pressure difference between the exhaust and ambient air is 1.85 × 104? The exhaust area is 2m2, the ambient and exhaust velocities are 280 m/s and 400 m/s.

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Thrust is the force applied to an aircraft in the direction of flight. Jet engines produce thrust by: Mixing fuel with oxygen or another oxidizer in a combustion chamber Igniting the mixture Creating hot, expanding gases Using the expanding gases to produce thrust directly  Jet engines produce thrust in a similar way to the engine/propeller combination. Both propel the aircraft by thrusting a large weight of air backwards: One in the form of a large air slipstream at comparatively low speed The other in the form of a jet of gas at very high speed  Jet engines commonly develop 9,900... Show more

What is the thrust of an engine if the inlet and exhaust mass flow rate are 150 kg/s and 190 kg/s respectively with the pressure difference between the exhaust and ambient air is 1.85 × 10<sup>4</sup>? The exhaust area is 2m<sup>2</sup>, the ambient and exhaust velocities are 280 m/s and 400 m/s.






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