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Which factor must be reduced in cruise method 3?

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in Aircraft Performance by (558k points)
Which factor must be reduced in cruise method 3?

(a) Mach number

(b) Angle of attack

(c) Altitude

(d) Temperature

I had been asked this question in class test.

The above asked question is from Cruise Method 3 topic in portion Cruising Performance of Aircraft Performance

1 Answer

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Correct option is (b) Angle of attack

Explanation: The factor that must be reduced in cruise method 3 (also known as constant mach number and constant altitude method) is angle of attack. Also the ratio of weight to lift coefficient and relative airspeed are kept constant i.e. W/CL ratio and u are constant throughout the method.

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