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AT116 Exam 2 2022 Study Guide with Complete Solutions

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AT116 Exam 2 2022 Study Guide with Complete Solutions Why would we want anhedral on a wing? - Answer-The a/c has a very heavy and low center of gravity Which of the following is NOT one of the ways an airplane gains stability around vertical axis? - Answer-Move CG behind center of lift How do...

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  • October 2, 2024
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AT116 Exam 2 2022 Study Guide with
Complete Solutions

Why would we want anhedral on a wing? - Answer✔✔-The a/c has a very heavy and low center of

gravity


Which of the following is NOT one of the ways an airplane gains stability around vertical axis? -

Answer✔✔-Move CG behind center of lift


How do we create yaw stability on an a/c? - Answer✔✔-Only a & b are correct


Put a vertical stabilizer on tail of a/c


Sweep wings back


What produces pitch stability on a standard a/c? - Answer✔✔-Both b & c are correct


Horizontal stabilizer pulls downward


Horizontal stabilizer constantly changes AOA w/ pitch to dampen pitching motion


T/F: Pitch Stability is considered to be longitudinal stability - Answer✔✔-True


T/F: Wing dihedral is one of the ways we achieve stability around longitudinal axis - Answer✔✔-True


T/F: Wing dihedral must be greater on high wing a/c than on a low wing a/c - Answer✔✔-False


How does dihedral make an a/c stable? - Answer✔✔-The wing that falls, results in a Bernoulli force that

directly opposes gravity, and lifts the wing back up


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FIRST PUBLISH SEPTEMBER 2024


T/F: High wing a/c have natural stability because the CG is below lift - Answer✔✔-True


Which of the following is NOT one of the ways that swept back wings provide yaw stability for an a/c that

inadvertently yaws to the right? - Answer✔✔-The wing left wing tip produces more induced drag and

that pulls the a/c back left


Which of the following is NOT an advantage of a high wing a/c? - Answer✔✔-Easier to build strong

landing gear support


Which of the following is NOT an advantage of a low wing a/c? - Answer✔✔-Better lift/drag ratio


What causes ground effect in a fixed wing a/c? - Answer✔✔-Air gets trapped under the wing and

artificially raises the pressure under the wing


Which of the following is true of a SPIN? - Answer✔✔-All answers are correct


What is the advantage of a Vee Tail? - Answer✔✔-It reduces drag


Why is a Tee Tail considered to be better at high angles of attack? - Answer✔✔-The horizontal stabilizer

does not block the flow of air over the rudder.


Why is a Tee Tail considered undesirable? - Answer✔✔-The vertical stabilizer must be thicker and heavier

to support the horizontal stabilizer


If you wish to yaw a vee tail a/c to the left, what is the correct position of the flight controls on the tail? -

Answer✔✔-Right ruddervator up, left ruddervator down (Whichever yaw direction is, that ruddervator is

down)




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