turbojet u rečniku PONS

Jednojezični primeri (nisu ih verifikovali PONS urednici)

engleski
The exhaust nozzle forked in two at the end of the turbojet engine and ended in two auxiliary combustion chambers located on the trailing edges of the circular wing.
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Postwar commercial airframe design focused on larger capacities, on turboprop engines, and then on jet (turbojet, later turbofan) engines.
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The single turbojet engine was fed by cheek intakes.
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These initial aspects are very similar to how a turbojet operates, however, there are several differences.
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A turbojet engine sustained the long-range cruise flight after the boosters were dropped.
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Designing a basic turbojet engine around the second principle produces the turbofan engine, which creates slower gas but more of it.
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A turbojet engine equipped with an afterburner is called an afterburning turbojet, whereas a turbofan engine similarly equipped is sometimes called an augmented turbofan.
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Low bypass turbofans have a lower exhaust speed than turbojets and are mostly used for high sonic and transonic and low supersonic speeds.
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Aside from giving faster flight speeds turbojets had greater reliability than piston engines, with some models demonstrating dispatch reliability rating in excess of 99.9%.
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The fuel ignited when it came in contact with the hot components of the turbojet engine, forcing the pilot to trade speed for altitude, climb and bail out.
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