The asymmetric blade effect occursQuestion 39Select one:a.When the propeller over speeds in a high speed diveb.When the aircraft is operating at 40 angle of attackc.With all aircraft during take-offd.Only during take-off in a tail wheel aircraft

For takeoff, the blade angle of a constant speed propeller should be set at an angle which producesQuestion 13Select one:a.Equal pressure on each side of the bladeb.A small angle of attackc.A large angle of attackd.High drag forces on the propeller

For take-off the CSU would automatically set the blade angle of a constant speed propeller at an angle which producesQuestion 8Select one:a.Equal pressure on each side of the bladeb.High drag forces on the propeller to increase power available in the climbc.A large angle of attackd.A small angle of attack

The propeller blade section angle varies from the hub to the tip so that there isQuestion 6Select one:a.An increase in the angle from hub to tipb.A decrease in the angle from hub to tip

One way a CSU propeller achieves higher efficiency than a fixed pitch propeller is byQuestion 33Select one:a.Increasing the propeller pitch as speed increases during a take-off to maintain a constant angle of attackb.Increasing the propeller pitch as speed increases during a take-off to increase the angle of attackc.Decreasing the propeller pitch as speed increases during a take-off to maintain a small propeller angle of attackd.Decreasing the propeller pitch as speed increases during a take-off to maintain a constant angle of attack

The relationship between blade angle and propeller pitch for a variable pitch propeller is such that if the blade angle is increased, the pitch of the propeller willQuestion 30Select one:a.Increaseb.Decreasec.Remain constantClear my choice