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

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

Propeller torque is theQuestion 25Select one:a.Aerodynamic force acting at right angles to the thrust force and acting in the same direction as the rotation of the propellerb.Force tending to rotate the blade into a different pitchc.Force acting at right angles to the thrust force and acting in the opposite direction to the rotation of the propellerd.Aerodynamic force acting parallel but opposite to the path of the blade section

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