UAV Loading and Performance

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.

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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

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.

UAV Loading and Performance

During an approach to a stall, an increased load factor will cause the aircraft to

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

The angle of attack at which an airplane wing stalls will

In a fixed-wing aircraft, roll is controlled by

What could be a consequence of operating a small unmanned aircraft above its maximum allowable weight?

The acute angle A is the angle of

If an unmanned airplane weighs 33 pounds, what approximate weight would the airplane structure be required to support during a 30° banked turn while maintaining altitude?

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

In a fixed-wing aircraft, yaw is controlled by

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

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UAV Loading and Performance

UAV Loading and Performance

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