Which statement is correct about the flow in a divergent jet engine inlet I The static pressure remains constant in flow direction II The total temperature remains constant in flow direction ? Experience > lift > off
Which of these statements about compressor stall are correct or incorrect I A compressor stall is most likely to occur in a compressor designed for a high pressure ratio operating at low RPM II A ?
In a compressor stage if the axial air velocity increases more than the rotor blade velocity the ?
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1299 Free Training Exam