39. The primary advantage of an axial-flow compressor over a centrifugal compressor is (A)lager frontal area. (B)less expensive. (C)greater pressure ratio. (D)light weight

5. If an aircraft is operating at 40,000 ft. the pressurization ensures that (A)sea level pressure is maintained in the cabin. (B)the cabin pressure is progressively increased until the operational height is reached. (C)the cabin pressure above 10,000 ft. (D)the cabin pressure is equivalent to an altitude of less than 10,000 ft.

39. The primary advantage of an axial-flow compressor over a centrifugal compressor is
(A)lager frontal area.
(B)less expensive.
(C)greater pressure ratio.
(D)light weight

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