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jet engine and water intake.
im more curious about this that it being a must know thing.
how much water can a jet engine draw in before it stalls ? ive never one read of a jet engine stalling because it goes through a storm of storm cloud. the way a jet engine works it would suck possably tons of water in to the intakes at maximum engine speed/air speed.
anyone ?
Answers
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For more on marking an answer as the "Best Answer", please visit our FAQ.I presume they are tested for such things as you wouldn't want the fire going out as you're hurtling at 200MPH towards the end of the runway!
I believe some jet engines have/had deliberate water injection to temporarily increase the thrust. (It expands to steam)
Firstly, this video might be educational: http://www.geae.com/education/engines101/popups/mov_wateringestion.html
This is a required test for certification of the engine. The quantity of water used is huge, but I don't have the quantitiy figures at hand.
Secondly, the newer high-by pass ratio turbo fans could actually take even more water since, as the name implies, the large shrouded fan at the front of the engine bypasses a lot of the incoming air and acts as a propeller, giving the engine more efficiency, especially at the lower take-off speeds.
The take-off ingestion of standing water is ameliorated by the design of the nose gear "chined tires". There's a pronounced rubber "rim" near the tread of the tire that flares the water out and away form the intakes of the engines. This, is in addition to deflector vanes attached to various locations on the forward fuselage. One final design feature is the use of continuous ignition selection when in heavy turbulence and rain/precipitation. (Normally, the ignition is turned off).
Additional info on casto's comment on water injection,
The injected water vaporises and cools down the air through the intake which in turn increases the density of the mass flow air into the engine. With this increase of mass flow into the engine there can be a increase of fuel to maintain the Stoiciometric Ratio ( 15/1 Air to fuel mix). This is how extra thrust is obtained.
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