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Divided entrance duct
On a single engine aircraft with fuselage mounted engines, either a wing root inlet or a side scoop inlet may be used. The wing root inlet presents a problem to designers in the forming of the curvature necessary to deliver the air to the engine compressor. The side scoop inlet is placed as far forward of the compressor as possible to approach the straight line effect of the single inlet. Both types suffer faults, in a yaw or turn, a loss of ram pressure occurs on one side of the intake and separated, turbulent boundary layer air is fed to the engine compressor.
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Procedures for starting and ground running: Before starting and ground running any gas turbine powered aircraft, several considerations must be taken into account. The first an
Non-discounted cash flow method, Payback period method In this method, time value of money is not considered. It takes into account the number of years required to recover the in
WORKING OF I.C. ENGINE Basically there are 2 types of internal combustion engines; the two stoke type and the 4-stroke type. A brief description of these is given below: 1.
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FIRING ORDER If in multi cylinder engines, various cylinders are made to fire one after the other, interference between adjacent cylinders would occur, since these may have o
explain electrometallurgy for metal extraction process using a schematic diagram
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(a) A section of road has a free flow speed of 55km/h and a jam density of 367 vehicles per kilometre. Assuming under a linear speed-density relationship, calculate the density at
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