UAV Loading and Performance – UAV Campus | Remote Pilot FAA Exam Prep for Drones

Sign Up

Sign Up to our FAA Prep for the Remote Pilot Exam. Ask questions, answer people’s questions, and connect with other UAV/Drone Pilots.

Sign In

Login to our social questions & Answers Engine to ask questions answer people’s questions & connect with other people.

Forgot Password

Lost your password? Please enter your email address. You will receive a link and will create a new password via email.

You must login to ask a question.

Please briefly explain why you feel this question should be reported.

Please briefly explain why you feel this answer should be reported.

Please briefly explain why you feel this user should be reported.

Search

Ask A Question

1

UAV CampusAdministrator

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

As speed increases, induced drag will

1

remain constant. decrease. increase.

1

UAV CampusAdministrator

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

As temperature decreases, aircraft performance will

1

remain constant. decrease. increase.

1

UAV CampusAdministrator

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

An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be

1

stalling at higher-than-normal airspeed. a longer takeoff run. difficulty in recovering from a stalled condition.

0

UAV CampusAdministrator

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

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

0

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.

0

UAV CampusAdministrator

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

As the angle of attack increases, induced drag will

0

remain the same. increase. decrease.

0

UAV CampusAdministrator

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

The angle of attack at which an airplane wing stalls will

0

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

0

UAV CampusAdministrator

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

The acute angle A is the angle of

0

Attack. Dihedral. Incidence.

0

UAV CampusAdministrator

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

In a fixed-wing aircraft, yaw is controlled by

0

the rudder. the ailerons. the stabilizer.

0

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

0

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

0

UAV CampusAdministrator

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

In a fixed-wing aircraft, roll is controlled by

0

the stabilizer. the ailerons. the rudder.