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

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?

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  34 pounds. 38 pounds.  47 pounds.

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

When loading cameras or other equipment on an sUAS, mount the items in a manner that

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can be easily removed without the use of tools. is visible to the visual observer or other crew members. does not adversely affect the center of gravity.

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