Which statement is correct for a gas turbine engine with a constant speed propeller and free power turbine when the power setting is decreased I The HP spool speed decreases II The EGT decreases ? Students > orientation
The FADEC of a gas turbine engine consists of ?
The bypass ratio I is the ratio of inlet air mass flow to exhaust air mass flow II can be determined from the bypass air mass flow and the HP compressor mass flow ?
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1279 Free Training Exam