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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.
Boroscope inspections: Boroscope inspections involve looking at components within an engine using an optical probe. The probes are inserted in to the engine through ports in th
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Thrust reversal: Thrust reversal is a means of reducing the landing run of an aircraft without excessive use of wheel brakes or the use of braking parachutes. On a propeller d
Turbo shaft engines : Gas turbine engines that deliver power through a shaft to operate something other than a propeller are referred to as turboshaft engines. In most cases th
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Estimators for control: Applying control by the state itself needs transducers measuring each componentof x. If instead we apply control using the estimate of state (as prov
Thin-skinned Structures The SCB geometry can't be used because the skins are too flexible. Instead, a centre-notch flexure (CNF) test can be used. A hole is drilled abo
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