UAV Loading and Performance

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

The term “angle of attack” is defined as the angle between the

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airplane’s center line and the relative wind. chord line of the wing and the relative wind. airplane’s longitudinal axis and that of the air striking the airfoil.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

As the angle of attack increases, induced drag will

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remain the same. increase. decrease.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

The angle of attack at which an airplane wing stalls will

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increase if the CG is moved forward. remain the same regardless of gross weight. change with an increase in gross weight.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

The acute angle A is the angle of

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Attack. Dihedral. Incidence.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

In a fixed-wing aircraft, yaw is controlled by

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the rudder. the ailerons. the stabilizer.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

To ensure that the unmanned aircraft center of gravity (CG) limits are not exceeded, follow the aircraft loading instructions specified in the

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Aircraft Weight and Balance Handbook. Aeronautical Information Manual (AIM). Pilot’s Operating Handbook or UAS Flight Manual.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

In a fixed-wing aircraft, roll is controlled by

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the stabilizer. the ailerons. the rudder.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

According to 14 CFR part 107, who is responsible for determining the performance of a small unmanned aircraft?

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Remote Pilot in Command Manufacturer. Owner or operator

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

In a fixed-wing aircraft, pitch is controlled by

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the rudder. the ailerons. the stabilizer.

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UAV CampusAdministrator

Asked: May 31, 2024In: UAV Loading and Performance

When operating an unmanned airplane, the remote pilot should consider that the load factor on the wings may be increased anytime

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the CG is shifted rearward to the aft CG limit. the gross weight is reduced. the airplane is subjected to maneuvers other than straight and level flight.