fuel flows in a 3 5 m pipe from a fuel tank to the pump of a jet engin
Fuel flows in a 3.5-m pipe from a fuel tank to the pump of a jet engine. The
flow rate is 200 1/min. At high altitudes the fuel-tank pressure is low, and
there may be considerable danger of the fuel "boiling" or cavitating as it
enters the pump. In such a case the pump would be vapor locked and would
cease to deliver fuel to the engine. Show qualitatively how the pressure drop
in the line varies with its diameter (over a wide range). What would the mini-
mum pipe diameter be if a pipe pressure loss of only 3 kPa were tolerable?
The pipe has no sharp bends or elbows.
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